-
2
-
-
57549109455
-
-
Mack, L. M., Boundary Layer Linear Stability Theory, Special Course on Stability and Transition of Laminar Flow, AGARD, Rept. 709, Neuilly-sur-Seine, France, Mar. 1984, pp. 1-81.
-
Mack, L. M., "Boundary Layer Linear Stability Theory," Special Course on Stability and Transition of Laminar Flow, AGARD, Rept. 709, Neuilly-sur-Seine, France, Mar. 1984, pp. 1-81.
-
-
-
-
3
-
-
0038805681
-
Stability and Transition of Three-Dimensional Boundary Layers
-
doi:10.1146/annurev.fluid.35.101101. 161045
-
Saric, W. S., Reed, H. L., and White, E. B., "Stability and Transition of Three-Dimensional Boundary Layers," Annual Review of Fluid Mechanics, Vol. 35, 2003, pp. 413-440. doi:10.1146/annurev.fluid.35.101101. 161045
-
(2003)
Annual Review of Fluid Mechanics
, vol.35
, pp. 413-440
-
-
Saric, W.S.1
Reed, H.L.2
White, E.B.3
-
4
-
-
0033873396
-
Laminar-Turbulent Transition Prediction in Three-Dimensional Flows
-
Feb, doi: 10.1016/S0376-0421(00)00002-6
-
Amal, D., and Casalis, G., "Laminar-Turbulent Transition Prediction in Three-Dimensional Flows," Progress in Aerospace Sciences, Vol. 36, No. 2, Feb. 2000, pp. 173-191. doi: 10.1016/S0376-0421(00)00002-6
-
(2000)
Progress in Aerospace Sciences
, vol.36
, Issue.2
, pp. 173-191
-
-
Amal, D.1
Casalis, G.2
-
5
-
-
2342470027
-
-
Reshotko, Eli., and Tumin, Anatoli., Role of Transient Growth in Roughness-Induced Transition, AIAA Journal, 42, No. 4, Apr. 2004, pp. 766-770. 10.2514/1.9558
-
Reshotko, Eli., and Tumin, Anatoli., "Role of Transient Growth in Roughness-Induced Transition," AIAA Journal, Vol. 42, No. 4, Apr. 2004, pp. 766-770. 10.2514/1.9558
-
-
-
-
6
-
-
57549116655
-
-
AGARD, Rept. AG4/M4, Neuilly-sur-Seine, France, Sept
-
Abbott, Ira H., "Some Factors Contributing to Scale Effect at Supersonic Speeds," AGARD, Rept. AG4/M4, Neuilly-sur-Seine, France, Sept. 1953.
-
(1953)
Some Factors Contributing to Scale Effect at Supersonic Speeds
-
-
Abbott, I.H.1
-
7
-
-
0035332207
-
Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
-
May-June, doi:10.2514/2.3705
-
Schneider, S. P., "Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition," Journal of Spacecraft and Rockets, Vol. 38, No. 3, May-June 2001, pp. 323-333. doi:10.2514/2.3705
-
(2001)
Journal of Spacecraft and Rockets
, vol.38
, Issue.3
, pp. 323-333
-
-
Schneider, S.P.1
-
8
-
-
78149423047
-
-
Borg, Matthew P., Schneider, S. P., and Juliano, T. J., Effect of Freestream Noise on Roughness-Induced Transition for the X-51A Forebody, AIAA Paper 2008-0592, Jan. 2008.
-
Borg, Matthew P., Schneider, S. P., and Juliano, T. J., "Effect of Freestream Noise on Roughness-Induced Transition for the X-51A Forebody," AIAA Paper 2008-0592, Jan. 2008.
-
-
-
-
9
-
-
48849093512
-
Development of Hypersonic Quiet Tunnels
-
July-Aug, doi:10.2514/1.34489
-
Schneider, S. P., "Development of Hypersonic Quiet Tunnels," Journal of Spacecraft and Rockets, Vol. 45, No. 4, July-Aug. 2008, pp. 641-664. doi:10.2514/1.34489
-
(2008)
Journal of Spacecraft and Rockets
, vol.45
, Issue.4
, pp. 641-664
-
-
Schneider, S.P.1
-
10
-
-
78049516003
-
Effect of Freestream Noise on Roughness-Induced Transition at Mach 6
-
AIAA Paper 2008-4291, June
-
Casper, K. M., Wheaton, B. M., Johnson, H. B., and Schneider, S. P., "Effect of Freestream Noise on Roughness-Induced Transition at Mach 6," AIAA Paper 2008-4291, June 2008.
-
(2008)
-
-
Casper, K.M.1
Wheaton, B.M.2
Johnson, H.B.3
Schneider, S.P.4
-
11
-
-
33846116031
-
-
Schneider, S. P., Laminar-Turbulent Transition on Reentry Capsules and Planetary Probes, Journal of Spacecraft and Rockets, 43, No. 6, Nov.-Dec. 2006, pp. 1153-1173; also Erratum 44, No. 2, Mar.-Apr. 2007, pp. 464-484. doi:10.2514/1.30727
-
Schneider, S. P., "Laminar-Turbulent Transition on Reentry Capsules and Planetary Probes," Journal of Spacecraft and Rockets, Vol. 43, No. 6, Nov.-Dec. 2006, pp. 1153-1173; also Erratum Vol. 44, No. 2, Mar.-Apr. 2007, pp. 464-484. doi:10.2514/1.30727
-
-
-
-
12
-
-
0032715875
-
Flight Data for Boundary-layer Transition at Hypersonic and Supersonic Speeds
-
doi:10.2514/2.3428
-
Schneider, S. P., "Flight Data for Boundary-layer Transition at Hypersonic and Supersonic Speeds," Journal of Spacecraft and Rockets, Vol. 36, No. 1, 1999, pp. 8-20. doi:10.2514/2.3428
-
(1999)
Journal of Spacecraft and Rockets
, vol.36
, Issue.1
, pp. 8-20
-
-
Schneider, S.P.1
-
13
-
-
1342283922
-
Hypersonic Laminar-Turbulent Transition on Circular Cones and Scramjet Forebodies
-
doi: 10.1016/j.paerosci.2003.11. 001
-
Schneider, S. P., "Hypersonic Laminar-Turbulent Transition on Circular Cones and Scramjet Forebodies," Progress in Aerospace Sciences, Vol. 40, No. 1-2, 2004, pp. 1-50. doi: 10.1016/j.paerosci.2003.11. 001
-
(2004)
Progress in Aerospace Sciences
, vol.40
, Issue.1-2
, pp. 1-50
-
-
Schneider, S.P.1
-
14
-
-
42949166155
-
Effects of Roughness on Hypersonic BoundaryLayer Transition
-
Mar.-Apr, doi: 10.2514/1.29713
-
Schneider, S. P., "Effects of Roughness on Hypersonic BoundaryLayer Transition," Journal of Spacecraft and Rockets, Vol. 45, No. 2, Mar.-Apr. 2008, pp. 193-209. doi: 10.2514/1.29713
-
(2008)
Journal of Spacecraft and Rockets
, vol.45
, Issue.2
, pp. 193-209
-
-
Schneider, S.P.1
-
15
-
-
85003237321
-
Correlation of Nosetip Boundary-layer Transition Data Measured in Ballistics-Range Experiments
-
Mar, doi:10.2514/3.50952
-
Reda, D. C., "Correlation of Nosetip Boundary-layer Transition Data Measured in Ballistics-Range Experiments," AIAA Journal, Vol. 19, No. 3, Mar. 1981, pp. 329-339. doi:10.2514/3.50952
-
(1981)
AIAA Journal
, vol.19
, Issue.3
, pp. 329-339
-
-
Reda, D.C.1
-
16
-
-
0036493808
-
Review and Synthesis of Roughness-Dominated Transition Correlations for Reentry Applications
-
Mar.-Apr, doi:10.2514/2.3803
-
Reda, D. C., "Review and Synthesis of Roughness-Dominated Transition Correlations for Reentry Applications," Journal of Space-craft and Rockets, Vol. 39, No. 2, Mar.-Apr. 2002, pp. 161-167. doi:10.2514/2.3803
-
(2002)
Journal of Space-craft and Rockets
, vol.39
, Issue.2
, pp. 161-167
-
-
Reda, D.C.1
-
17
-
-
0020543185
-
-
Batt, R. G., and Legner, H. H., A Review of Roughness-Induced Nosetip Transition, AIAA Journal, 21, No. 1, Jan. 1983, pp. 7-22; also AIAA Paper 81-1223, June 1981.
-
Batt, R. G., and Legner, H. H., "A Review of Roughness-Induced Nosetip Transition," AIAA Journal, Vol. 21, No. 1, Jan. 1983, pp. 7-22; also AIAA Paper 81-1223, June 1981.
-
-
-
-
20
-
-
78049490706
-
Hypersonic Boundary-Layer Transition with Ablation and Blowing
-
AIAA Paper 2008-3730, June
-
Schneider, S. P., "Hypersonic Boundary-Layer Transition with Ablation and Blowing," AIAA Paper 2008-3730, June 2008.
-
(2008)
-
-
Schneider, S.P.1
-
21
-
-
78149445601
-
Protuberance Boundary Layer Transition for Project Orion Crew Entry Vehicle
-
Jan
-
Amar, A. J., Horvath, T. J., Hollis, B. R., Berger, K. T., Berry, S. A., and Calvert, N., "Protuberance Boundary Layer Transition for Project Orion Crew Entry Vehicle," AIAA, Paper 2008-1227, Jan. 2008.
-
(2008)
AIAA, Paper
, vol.2008 -1227
-
-
Amar, A.J.1
Horvath, T.J.2
Hollis, B.R.3
Berger, K.T.4
Berry, S.A.5
Calvert, N.6
-
22
-
-
84884950446
-
Laminar-Turbulent Transition on Reentry Capsules and Planetary Probes
-
AIAA Paper 2005-4763, June
-
Schneider, S. P., "Laminar-Turbulent Transition on Reentry Capsules and Planetary Probes," AIAA Paper 2005-4763, June 2005.
-
(2005)
-
-
Schneider, S.P.1
-
23
-
-
57549116658
-
-
Experimental Heat Transfer and Pressure Distributions over Entry Configurations of 0.02-Scale Apollo Models H-I and PS-I and Hemisphere-Cylinders at Mach Number of 10, NASA CR 117543, Jan. 1963; also North American Aviation, Inc., Space and Information Div., Rept. SID-63-623, Downey, CA, 1963.
-
"Experimental Heat Transfer and Pressure Distributions over Entry Configurations of 0.02-Scale Apollo Models H-I and PS-I and Hemisphere-Cylinders at Mach Number of 10," NASA CR 117543, Jan. 1963; also North American Aviation, Inc., Space and Information Div., Rept. SID-63-623, Downey, CA, 1963.
-
-
-
-
25
-
-
57549109659
-
-
NASA TM, July
-
Miller, C. G., III, and Lawing, P. L., "Experimental Investigation of Flow Characteristics of the Apollo Reentry Configuration at a Mach Number of 20 in Nitrogen," NASA TM-X-1258, July 1966.
-
(1966)
Experimental Investigation of Flow Characteristics of the Apollo Reentry Configuration at a Mach Number of 20 in Nitrogen
-
-
Miller III, C.G.1
Lawing, P.L.2
-
27
-
-
57549118903
-
Apollo Afterbody Heat Transfer and Pressure with and Without Ablation at Mach 5.8 to 8.3
-
NASA TND-3620, Sept
-
Lee, G., and Sundell, R. E., "Apollo Afterbody Heat Transfer and Pressure with and Without Ablation at Mach 5.8 to 8.3," NASA TND-3620, Sept. 1966.
-
(1966)
-
-
Lee, G.1
Sundell, R.E.2
-
30
-
-
57549107687
-
-
CR-117702, NASA, Aug, also North American Aviation, Inc, Space and Information Div, Rept. SID-62-1072, Downey, CA
-
Gorowitz, H., "NAA Shock Tunnel Tests /St-4/ of Apollo Command Modules H-6 and PS-6," CR-117702, NASA, Aug. 1962; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-1072, Downey, CA, 1962.
-
(1962)
NAA Shock Tunnel Tests /St-4/ of Apollo Command Modules H-6 and PS-6
-
-
Gorowitz, H.1
-
33
-
-
57549095199
-
-
Arnold Engineering Development Center, TR 68-224, Tullahoma, TN, Jan
-
Lawrence, W. R., and Norman, W. S., "Free-Flight Range Tests of the Apollo Command Module," Arnold Engineering Development Center, TR 68-224, Tullahoma, TN, Jan. 1969.
-
(1969)
Free-Flight Range Tests of the Apollo Command Module
-
-
Lawrence, W.R.1
Norman, W.S.2
-
34
-
-
33846093617
-
The Effect of Protuberances, Cavities, and Angle of Attack on the Wind-Tunnel Pressure and Heat-Transfer Distribution for the Apollo Command Module
-
Bertin, J. J., "The Effect of Protuberances, Cavities, and Angle of Attack on the Wind-Tunnel Pressure and Heat-Transfer Distribution for the Apollo Command Module," NASA TM-X-1243, Get. 1966.
-
(1966)
NASA TM-X-1243, Get
-
-
Bertin, J.J.1
-
35
-
-
57549106820
-
-
Biss, W. J., and Emerson, D. X., Experimental Heat Transfer Distributions over Launch andEntry Configurations of an 0.045 Scale Apollo Model /H-2/ at Mach Numbers of 8 and 10, NASA CR-117538, Sept. 1962; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-993-VCL-1, Downey, CA, 1962.
-
Biss, W. J., and Emerson, D. X., "Experimental Heat Transfer Distributions over Launch andEntry Configurations of an 0.045 Scale Apollo Model /H-2/ at Mach Numbers of 8 and 10," NASA CR-117538, Sept. 1962; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-993-VCL-1, Downey, CA, 1962.
-
-
-
-
36
-
-
57549083074
-
Experimental Heat Transfer Distributions over the 0.090-Scale Apollo Command Module /H-11/ with Protuberances at Mach Number 10
-
NASA CR-117540, Nov
-
Emerson, R. X., "Experimental Heat Transfer Distributions over the 0.090-Scale Apollo Command Module /H-11/ with Protuberances at Mach Number 10," NASA CR-117540, Nov. 1964.
-
(1964)
-
-
Emerson, R.X.1
-
37
-
-
78149456959
-
Heat Transfer Tests of the 0.090-Scale Apollo Entry Configuration /H-11/ in the AEDC-VKF Hypersonic Tunnel C
-
June
-
Emerson, R. X., "Heat Transfer Tests of the 0.090-Scale Apollo Entry Configuration /H-11/ in the AEDC-VKF Hypersonic Tunnel C.," NASA CR-154529 June 1964.
-
(1964)
NASA CR-154529
-
-
Emerson, R.X.1
-
40
-
-
0001260917
-
Laminar Heat Transfer over Blunt-Nosed Bodies at Hypersonic Flight Speeds
-
Apr
-
Lees, L., "Laminar Heat Transfer over Blunt-Nosed Bodies at Hypersonic Flight Speeds," Jet Propulsion, Vol. 26, pp. 259-269, Apr. 1956.
-
(1956)
Jet Propulsion
, vol.26
, pp. 259-269
-
-
Lees, L.1
-
41
-
-
57549100624
-
-
NASA TM, Mar
-
Jones, R. A., and Hunt, J. L., "Effects of Cavities, Protuberances, and Reaction-Control Jets on Heat Transfer to the Apollo Command Module," NASA TM-X-1063, Mar. 1965.
-
(1965)
Effects of Cavities, Protuberances, and Reaction-Control Jets on Heat Transfer to the Apollo Command Module
-
-
Jones, R.A.1
Hunt, J.L.2
-
42
-
-
57549098407
-
Effects of Several Ramp-Fairing, Umbilical, and Pad Configurations on Aerodynamics Heating to Apollo Command Module at Mach 8
-
NASA TM-X-1640, Sept
-
Hunt, J. L., and Jones, R. A., "Effects of Several Ramp-Fairing, Umbilical, and Pad Configurations on Aerodynamics Heating to Apollo Command Module at Mach 8," NASA TM-X-1640, Sept. 1968.
-
(1968)
-
-
Hunt, J.L.1
Jones, R.A.2
-
43
-
-
57549105466
-
Recent Experimental Studies on Heat Transfer to Apollo Command Module
-
NASA, Jan
-
Jones, R. A., and Hunt, J. L., "Recent Experimental Studies on Heat Transfer to Apollo Command Module," Conference on Langley Research Related to the Apollo Mission, NASA, Jan. 1965, pp. 9-18.
-
(1965)
Conference on Langley Research Related to the Apollo Mission
, pp. 9-18
-
-
Jones, R.A.1
Hunt, J.L.2
-
44
-
-
57549091777
-
-
NASA, CR-153876, July, also North American Aviation, Inc, Space and Information Div, Rept. SID-63-44-R-3, Down, CA
-
"Apollo Wind Tunnel Model Nomenclature," NASA, CR-153876, July 1964; also North American Aviation, Inc., Space and Information Div., Rept. SID-63-44-R-3, Down, CA, 1963.
-
(1963)
Apollo Wind Tunnel Model Nomenclature
-
-
-
45
-
-
57549088675
-
-
NASA CR-156432, Feb, also North American Aviation, Inc, Space and Information Div, Rept. SID-62-170-4, Downey, CA
-
"Apollo Wind Tunnel Program. Report," NASA CR-156432, Feb. 1963; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-170-4, Downey, CA, 1962.
-
(1962)
Apollo Wind Tunnel Program. Report
-
-
-
46
-
-
57549103596
-
-
Apollo Wind Tunnel Program Report, NASA CR-156445, July 1963; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-170-5, Downey, CA, 1962.
-
"Apollo Wind Tunnel Program Report," NASA CR-156445, July 1963; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-170-5, Downey, CA, 1962.
-
-
-
-
47
-
-
57549099848
-
-
Udvardy, G. A., Data Report for Experimental Heat Transfer Distributions over Launch and Entry Configurations on the 0.045-Scale Apollo Model /H-2/ with, the Addition of Stakes at a Mach Number of 10, NASA CR-117230, Feb. 1.964; also North American Aviation, Inc., Space and Information Div., Rept. SID-63-1135-1, Downey, CA, 1963.
-
Udvardy, G. A., "Data Report for Experimental Heat Transfer Distributions over Launch and Entry Configurations on the 0.045-Scale Apollo Model /H-2/ with, the Addition of Stakes at a Mach Number of 10," NASA CR-117230, Feb. 1.964; also North American Aviation, Inc., Space and Information Div., Rept. SID-63-1135-VoL-1, Downey, CA, 1963.
-
-
-
-
48
-
-
57549095437
-
-
Experimental Heat Transfer Distributions over Launch and Entry Configurations on the 0.045-Scale Apollo Model /H-2/ with the Addition of Stakes at a Mach Number of 1.0, 3, NASA CR-116644, Feb. 1964; also North American Aviation, Inc., Space and Information Div., Rept. SID-63-1135-VCL-3, Downey, CA, 1963.
-
"Experimental Heat Transfer Distributions over Launch and Entry Configurations on the 0.045-Scale Apollo Model /H-2/ with the Addition of Stakes at a Mach Number of 1.0," Vol. 3, NASA CR-116644, Feb. 1964; also North American Aviation, Inc., Space and Information Div., Rept. SID-63-1135-VCL-3, Downey, CA, 1963.
-
-
-
-
49
-
-
57549101044
-
-
Experimental Heat Transfer Distributions over Launch And Entry Configurations on the 0.045-Scale Apollo Model /H-2/ with the Addition of Stakes at a Mach Number of 1.0, 6, NASA CR-116647, Feb. 1964; also North American Aviation, Inc., Space and Information Div., Rept. SID-63-1135-VCL-6, Downey, CA, 1963.
-
"Experimental Heat Transfer Distributions over Launch And Entry Configurations on the 0.045-Scale Apollo Model /H-2/ with the Addition of Stakes at a Mach Number of 1.0," Vol. 6, NASA CR-116647, Feb. 1964; also North American Aviation, Inc., Space and Information Div., Rept. SID-63-1135-VCL-6, Downey, CA, 1963.
-
-
-
-
50
-
-
57549097634
-
-
Biss, W. J., and Emerson, D. X., Experimental Heat Transfer Distributions over Launch and Entry Configurations of an 0.045 Scale Apollo Model /H-2/ at Mach. Numbers of 8 and 10, 3, NASA CR-11755.1, Sept. 1962; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-993-VCL-3-APP-A, Downey, CA, 1962.
-
Biss, W. J., and Emerson, D. X., "Experimental Heat Transfer Distributions over Launch and Entry Configurations of an 0.045 Scale Apollo Model /H-2/ at Mach. Numbers of 8 and 10," Vol. 3, NASA CR-11755.1, Sept. 1962; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-993-VCL-3-APP-A, Downey, CA, 1962.
-
-
-
-
51
-
-
57549113130
-
-
Biss, W. J., and Emerson, D. X., Experimental. Heat Transfer Distributions over Launch and Entry Configurations of an 0.045 Scale Apollo Model /H-2/ at Mach Numbers of 8 and 10, 6, NASA CR-1.17300, Sept. 1962; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-993-VCL-6-APP-B, Downey, CA, 1962.
-
Biss, W. J., and Emerson, D. X., "Experimental. Heat Transfer Distributions over Launch and Entry Configurations of an 0.045 Scale Apollo Model /H-2/ at Mach Numbers of 8 and 10," Vol. 6, NASA CR-1.17300, Sept. 1962; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-993-VCL-6-APP-B, Downey, CA, 1962.
-
-
-
-
52
-
-
57549085723
-
-
Biss, W. J., and Emerson, D. X., Experimental Heat Transfer Distributions over Launch and Entry Configurations of an 0.045 Scale Apollo Model /H-2/ at Mach Numbers of 8 and 1.0, 2, NASA CR-117542, Sept. 1962; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-993-VCL-2-APP-A, Downey, CA, 1962.
-
Biss, W. J., and Emerson, D. X., "Experimental Heat Transfer Distributions over Launch and Entry Configurations of an 0.045 Scale Apollo Model /H-2/ at Mach Numbers of 8 and 1.0," Vol. 2, NASA CR-117542, Sept. 1962; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-993-VCL-2-APP-A, Downey, CA, 1962.
-
-
-
-
53
-
-
57549104514
-
-
Biss, W. J., and Emerson, D. X., Experimental Heat Transfer Distributions over Launch and Entry Configurations of an 0.045 Scale Apollo Model /H-2/ at Mach Numbers of 8 and 10, 4, NASA CR-117555, Sept. 1962; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-993-VCL-4-APP-B, Downey, CA, 1962.
-
Biss, W. J., and Emerson, D. X., "Experimental Heat Transfer Distributions over Launch and Entry Configurations of an 0.045 Scale Apollo Model /H-2/ at Mach Numbers of 8 and 10," Vol. 4, NASA CR-117555, Sept. 1962; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-993-VCL-4-APP-B, Downey, CA, 1962.
-
-
-
-
54
-
-
57549117280
-
-
Biss, W. J., and Emerson, D. X., Experimental Heat Transfer Distributions over Launch and Entry Configurations of an 0.045 Scale Apollo Model /H-2/ at Mach Numbers of 8 and 10, 5, NASA CR-117297, Sept. 1962; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-993-VPL-5-APP-B, Downey, CA, 1962.
-
Biss, W. J., and Emerson, D. X., "Experimental Heat Transfer Distributions over Launch and Entry Configurations of an 0.045 Scale Apollo Model /H-2/ at Mach Numbers of 8 and 10," Vol 5, NASA CR-117297, Sept. 1962; also North American Aviation, Inc., Space and Information Div., Rept. SID-62-993-VPL-5-APP-B, Downey, CA, 1962.
-
-
-
-
55
-
-
57549083618
-
-
Wool, M. R., Passive Nosetip Technology (PANT) Program, 10: Summary of Experimental and Analytical Results, Space and Missile Systems Crganization TR-74-86-X, Los Angeles AFB, CA, Jan. 1975.
-
Wool, M. R., "Passive Nosetip Technology (PANT) Program, Volume 10: Summary of Experimental and Analytical Results," Space and Missile Systems Crganization TR-74-86-Vol-X, Los Angeles AFB, CA, Jan. 1975.
-
-
-
-
56
-
-
57549111273
-
-
Abbett, M. J., Anderson, A. D., Cooper, L., Dahm, T. J., Kelly, J., Gverly, P., and Sandhu, S., Passive Nosetip Technology (PANT) Program, 20: Investigation of Flow Phenomena over Reentry Vehicle Nosetips, Space and Missile Systems Crganization, TR-74-86-XX, Los Angeles AFB, CA, Aug. 1975.
-
Abbett, M. J., Anderson, A. D., Cooper, L., Dahm, T. J., Kelly, J., Gverly, P., and Sandhu, S., "Passive Nosetip Technology (PANT) Program, Volume 20: Investigation of Flow Phenomena over Reentry Vehicle Nosetips," Space and Missile Systems Crganization, TR-74-86-Vol-XX, Los Angeles AFB, CA, Aug. 1975.
-
-
-
-
57
-
-
57549117979
-
-
Jackson, M., D., Passive Nosetip Technology (PANT) Program, 1.5: Roughness Induced Transition on Blunt Axisymmetric Bodies, Space and Missile Systems Crganization TR-74-86-XV, Los Angeles AFB, CA, Apr. 1974.
-
Jackson, M., D., "Passive Nosetip Technology (PANT) Program, Volume 1.5: Roughness Induced Transition on Blunt Axisymmetric Bodies," Space and Missile Systems Crganization TR-74-86-Vol-XV, Los Angeles AFB, CA, Apr. 1974.
-
-
-
-
58
-
-
57549089608
-
Surface Roughness Effects on Nosetip Ablation Characteristics
-
AIAA Paper 74-513, June
-
Grabow, R. M., and White, C. P., "Surface Roughness Effects on Nosetip Ablation Characteristics," AIAA Paper 74-513, June 1974.
-
(1974)
-
-
Grabow, R.M.1
White, C.P.2
-
59
-
-
57549096902
-
-
Eitman, D. A., and DeMichaels, J. E., Performance Technology Program (PTP-S II), 10, U.S. Air Force Ballistic Missile Office, TR 80-40 BMO, Norton AFB, CA, Jan. 1980.
-
Eitman, D. A., and DeMichaels, J. E., "Performance Technology Program (PTP-S II)," Vol. 10, U.S. Air Force Ballistic Missile Office, TR 80-40 BMO, Norton AFB, CA, Jan. 1980.
-
-
-
-
60
-
-
0001858503
-
Bypass Transition to Turbulence and Research Desiderata
-
NASA CP-2386, May
-
Morkovin, M. V., "Bypass Transition to Turbulence and Research Desiderata," Transition in Turbines, NASA CP-2386, May 1984, pp. 161-199.
-
(1984)
Transition in Turbines
, pp. 161-199
-
-
Morkovin, M.V.1
-
61
-
-
57549111470
-
-
Morkovin, M. V., Critical Evaluation of Transition from Laminar to Turbulent Shear Layers with Emphasis on Hypersonically Traveling Bodies, U.S. Air Force Flight Dynamics Lab., TR 68-149, Wright-Patterson AFB, OH, Mar. 1969.
-
Morkovin, M. V., "Critical Evaluation of Transition from Laminar to Turbulent Shear Layers with Emphasis on Hypersonically Traveling Bodies," U.S. Air Force Flight Dynamics Lab., TR 68-149, Wright-Patterson AFB, OH, Mar. 1969.
-
-
-
-
62
-
-
33748070105
-
-
NASA Johnson Space Center, Rept. JSC-26528, Houston, TX, Feb
-
Stetson, K. F., "Boundary-Layer Transition on Blunt Configurations," NASA Johnson Space Center, Rept. JSC-26528, Houston, TX, Feb. 1994.
-
(1994)
Boundary-Layer Transition on Blunt Configurations
-
-
Stetson, K.F.1
-
63
-
-
85003324745
-
Re-Evaluation of Heat-Transfer Data Obtained in Flight Tests of Heat-Sink Shielded Re-Entry Vehicles
-
Jan, doi:10.2514/3.28385
-
Murphy, J. D., and Rubesin, M. W., "Re-Evaluation of Heat-Transfer Data Obtained in Flight Tests of Heat-Sink Shielded Re-Entry Vehicles," Journal of Spacecraft and Rockets, Vol. 3, No. 1, Jan. 1966, pp. 53-60. doi:10.2514/3.28385
-
(1966)
Journal of Spacecraft and Rockets
, vol.3
, Issue.1
, pp. 53-60
-
-
Murphy, J.D.1
Rubesin, M.W.2
-
64
-
-
57549111660
-
An Evaluation of Free-Flight Test Data for Aerodynamic Heating from Laminar, Turbulent, and Transitional Boundary Layers Part 2: The X-17 Re-Entry Body
-
Apr
-
Murphy, J. D., and Rubesin, M. W., "An Evaluation of Free-Flight Test Data for Aerodynamic Heating from Laminar, Turbulent, and Transitional Boundary Layers Part 2: The X-17 Re-Entry Body," NASA, CR-70931, Apr, 1965.
-
(1965)
NASA, CR-70931
-
-
Murphy, J.D.1
Rubesin, M.W.2
-
65
-
-
57549116515
-
-
Missile Systems Div, Lockheed Aircraft Corp, Rept. MSD-3003, Sunnyvale, CA, Apr
-
Balgeman, E. J., Cassell, G., Dension, M. R., and Tellep, D. M., "X-17 Re-Entry Test Vehicle: R-2 Final Flight Report," Missile Systems Div., Lockheed Aircraft Corp., Rept. MSD-3003, Sunnyvale, CA, Apr. 1957.
-
(1957)
X-17 Re-Entry Test Vehicle: R-2 Final Flight Report
-
-
Balgeman, E.J.1
Cassell, G.2
Dension, M.R.3
Tellep, D.M.4
-
66
-
-
57549111845
-
Correlation of Boundary-Layer Transition Results on Highly Cooled Blunt Bodies
-
Wisniewski, R. J., "Correlation of Boundary-Layer Transition Results on Highly Cooled Blunt Bodies," NASA, TM-X-412, Get. 1960.
-
(1960)
NASA, TM-X-412, Get
-
-
Wisniewski, R.J.1
-
67
-
-
57549116865
-
The Relation Between Wall Temperature and the Effect of Roughness on Boundary-Layer Transition
-
Aug
-
Potter, L. J., and Whitfield, J. D., "The Relation Between Wall Temperature and the Effect of Roughness on Boundary-Layer Transition," Journal of the Aerospace Sciences, Vol. 28, No. 8, Aug. 1961, pp. 663-664.
-
(1961)
Journal of the Aerospace Sciences
, vol.28
, Issue.8
, pp. 663-664
-
-
Potter, L.J.1
Whitfield, J.D.2
-
68
-
-
57549086850
-
-
Finson, M. L., An Analysis of Nosetip Boundary Layer Transition Data, Physical Sciences, Inc., Rept. PSI-TR-52, Woburn, MA, Aug. 1976; also U.S. Air Force Pffice of Scientific Research, Rept. AFPSR-TR-76-1106, Wright-Patterson AFB, PH, 1976.
-
Finson, M. L., "An Analysis of Nosetip Boundary Layer Transition Data," Physical Sciences, Inc., Rept. PSI-TR-52, Woburn, MA, Aug. 1976; also U.S. Air Force Pffice of Scientific Research, Rept. AFPSR-TR-76-1106, Wright-Patterson AFB, PH, 1976.
-
-
-
-
69
-
-
57549116513
-
-
Finson, M.L., Pirri, A.N., Nebolsine, P.E., Simons, G.A., and Wu, P. K. S., Advanced Reentiy Aeromechanics, Physical Sciences, Inc., Rept. PSI-TR-115, Woburn, MA, Jan. 1978; also U.S. Air Force Pffice of Scientific Research, Rept. AFPSR-TR-78-0607TR, Wright-Patterson AFB, OH, 1978.
-
Finson, M.L., Pirri, A.N., Nebolsine, P.E., Simons, G.A., and Wu, P. K. S., "Advanced Reentiy Aeromechanics," Physical Sciences, Inc., Rept. PSI-TR-115, Woburn, MA, Jan. 1978; also U.S. Air Force Pffice of Scientific Research, Rept. AFPSR-TR-78-0607TR, Wright-Patterson AFB, OH, 1978.
-
-
-
-
70
-
-
84975573319
-
Some Experiments at High Supersonic Speeds on the Aerodynamic and Boundary-Layer Transition Characteristics of High-Drag Bodies of Revolution
-
Jan
-
Seiff, A., Sommer, S., and Canning, T., "Some Experiments at High Supersonic Speeds on the Aerodynamic and Boundary-Layer Transition Characteristics of High-Drag Bodies of Revolution," NACA RM-A56I05, Jan. 1957.
-
(1957)
NACA RM-A56I05
-
-
Seiff, A.1
Sommer, S.2
Canning, T.3
-
71
-
-
57549117062
-
-
Cooper, M., and Mayo, E., Measurements of Local Heat Transfer and Pressure on. Six 2-Inch-Diameter Blunt Bodies at a Mach Number of 4.95 and at Reynolds Numbers per Foot Up to 81 × 10(exp 6), NASA TM-1-3-59L, Mar. 1959.
-
Cooper, M., and Mayo, E., "Measurements of Local Heat Transfer and Pressure on. Six 2-Inch-Diameter Blunt Bodies at a Mach Number of 4.95 and at Reynolds Numbers per Foot Up to 81 × 10(exp 6)," NASA TM-1-3-59L, Mar. 1959.
-
-
-
-
72
-
-
0842310156
-
Nosetip Bluntness Effects on Cone Frustum Boundary Layer Transition in Hypersonic Flow
-
AIAA Paper 83-1763, July
-
Stetson, K. F., "Nosetip Bluntness Effects on Cone Frustum Boundary Layer Transition in Hypersonic Flow," AIAA Paper 83-1763, July 1983.
-
(1983)
-
-
Stetson, K.F.1
-
73
-
-
57549096364
-
-
Bandettini, A., and Isler, W. E., Boundary-Layer Transition Measurements on Hemispheres of Various Surface Roughnesses in a Wind Tunnel at Mach Numbers from 2.48 to 3.55, NASA TM-12-25-58A, Mar. 1959.
-
Bandettini, A., and Isler, W. E., "Boundary-Layer Transition Measurements on Hemispheres of Various Surface Roughnesses in a Wind Tunnel at Mach Numbers from 2.48 to 3.55," NASA TM-12-25-58A, Mar. 1959.
-
-
-
-
74
-
-
85087101963
-
-
61, NASA TN-D-391, July 1960.
-
61," NASA TN-D-391, July 1960.
-
-
-
-
75
-
-
57549102590
-
-
NASA, TN-D-907, Aug
-
Deveikis, W. D., and Walker, R. W., "Local Aerodynamic Heat Transfer and Boundary-Layer Transition on Roughened Sphere-Ellipsoid Bodies at Mach Number 3.0," NASA, TN-D-907, Aug. 1961.
-
(1961)
Local Aerodynamic Heat Transfer and Boundary-Layer Transition on Roughened Sphere-Ellipsoid Bodies at Mach Number 3.0
-
-
Deveikis, W.D.1
Walker, R.W.2
-
76
-
-
57549095004
-
-
Jackson, M. W., and Czamecki, K. R., Boundary-Layer Transition on a Group of Blunt Nose Shapes at a Mach Number of 2.20, NASA, TN-D-932, July 1961.
-
Jackson, M. W., and Czamecki, K. R., "Boundary-Layer Transition on a Group of Blunt Nose Shapes at a Mach Number of 2.20," NASA, TN-D-932, July 1961.
-
-
-
-
77
-
-
0019545802
-
Correlation of Artificially Induced Boundary-Layer Transition Data at Hypersonic Speeds
-
Mar.-Apr, doi:10.2514/3.28053
-
Boudreau, A. H., "Correlation of Artificially Induced Boundary-Layer Transition Data at Hypersonic Speeds," Journal of Spacecraft and Rockets, Vol. 18, No. 2, Mar.-Apr. 1981, pp. 152-156. doi:10.2514/3.28053
-
(1981)
Journal of Spacecraft and Rockets
, vol.18
, Issue.2
, pp. 152-156
-
-
Boudreau, A.H.1
-
78
-
-
57549102272
-
-
NASA, TN-D-3871, Mar
-
Dunavant, J. C., and Stone, H. W., "Effect of Roughness on Heat Transfer to Hemisphere Cylinders at Mach Numbers 10.4 and 11.4," NASA, TN-D-3871, Mar. 1967.
-
(1967)
Effect of Roughness on Heat Transfer to Hemisphere Cylinders at Mach Numbers 10.4 and 11.4
-
-
Dunavant, J.C.1
Stone, H.W.2
-
79
-
-
85007721154
-
Boundary Layer Transition on Blunt Bodies-Effects of Roughness
-
Oct, doi:10.2514/3.4337
-
Van Driest, E. R., Blumer, C. B., and Wells, C. S., Jr., "Boundary Layer Transition on Blunt Bodies-Effects of Roughness," AIAA Journal, Vol. 5, Oct. 1967, pp. 1913-1915. doi:10.2514/3.4337
-
(1967)
AIAA Journal
, vol.5
, pp. 1913-1915
-
-
Van Driest, E.R.1
Blumer, C.B.2
Wells Jr., C.S.3
-
80
-
-
57549106818
-
-
Van Driest, E. R., and Blumer, C. B., Boundary Layer Transition on Cones and Spheres at Supersonic Speeds-Effects of Roughness and Cooling, U.S. Air Force Office of Scientific Research, Rept. 67-2048, Wright-Patterson AFB, OH, July 1967.
-
Van Driest, E. R., and Blumer, C. B., "Boundary Layer Transition on Cones and Spheres at Supersonic Speeds-Effects of Roughness and Cooling," U.S. Air Force Office of Scientific Research, Rept. 67-2048, Wright-Patterson AFB, OH, July 1967.
-
-
-
-
81
-
-
57549112933
-
-
Space and Missile Systems Organization, Rept. TR-70-229, Los Angeles AFB, CA, Apr
-
Varwig, R. L., "Effect of Roughness on Heating at the Forward Surface of a Sphere at Mach 5," Space and Missile Systems Organization, Rept. TR-70-229, Los Angeles AFB, CA, Apr. 1970.
-
(1970)
Effect of Roughness on Heating at the Forward Surface of a Sphere at Mach 5
-
-
Varwig, R.L.1
-
82
-
-
57549108673
-
-
Ross, D. H., Ellinwood, J. W., and Varwig, R. L., Hypersonic Shock Tunnel Transition Studies, Boundary Layer Transition Workshop, Aerospace Corp. Paper 8, Dec. 1971; also Aerospace Corp., Rept. TOR-0172(S2816-16)-5, San Bernardino, CA, Dec. 1971.
-
Ross, D. H., Ellinwood, J. W., and Varwig, R. L., "Hypersonic Shock Tunnel Transition Studies," Boundary Layer Transition Workshop, Aerospace Corp. Paper 8, Dec. 1971; also Aerospace Corp., Rept. TOR-0172(S2816-16)-5, San Bernardino, CA, Dec. 1971.
-
-
-
-
83
-
-
57549090226
-
Investigation of the Effects of Nose Bluntness on Natural and Induced Boundary-Layer Transition on Axisymmetric Bodies in Supersonic Flow
-
Tullahoma, TN, Feb
-
Coats, J. D., "Investigation of the Effects of Nose Bluntness on Natural and Induced Boundary-Layer Transition on Axisymmetric Bodies in Supersonic Flow," Arnold Engineering Development Center, AEDC-TR-73-36, Tullahoma, TN, Feb. 1973.
-
(1973)
Arnold Engineering Development Center, AEDC-TR-73-36
-
-
Coats, J.D.1
-
85
-
-
0017482656
-
-
Laderman, A. J., Effect of Surface Roughness on Blunt Body Boundary-Layer Transition, Journal of Spacecraft and Rockets, 1.4, No. 4, Apr. 1977, pp. 253-255. doi:10.2514/3.27968
-
Laderman, A. J., "Effect of Surface Roughness on Blunt Body Boundary-Layer Transition," Journal of Spacecraft and Rockets, Vol. 1.4, No. 4, Apr. 1977, pp. 253-255. doi:10.2514/3.27968
-
-
-
-
86
-
-
0016984980
-
Effect of Mass Addition on the Boundary Layer of a Hemisphere at Mach 6
-
Aug, doi:10.2514/3.27924
-
Demetriades, A., Laderman, A. J., Von Seggern, L., Hopkins, A. T., and Donaldson, J. C., "Effect of Mass Addition on the Boundary Layer of a Hemisphere at Mach 6," Journal of Spacecraft and Rockets, Vol. 13, No. 8, Aug. 1976, pp. 508-509. doi:10.2514/3.27924
-
(1976)
Journal of Spacecraft and Rockets
, vol.13
, Issue.8
, pp. 508-509
-
-
Demetriades, A.1
Laderman, A.J.2
Von Seggern, L.3
Hopkins, A.T.4
Donaldson, J.C.5
-
87
-
-
57549112555
-
Heat Transfer Studies on Ablation Protected Nosetips at Reentry Simulated Conditions
-
AIAA Paper 77-781, June
-
Richards, B. E., and DiCristina, V., "Heat Transfer Studies on Ablation Protected Nosetips at Reentry Simulated Conditions," AIAA Paper 77-781, June 1977.
-
(1977)
-
-
Richards, B.E.1
DiCristina, V.2
-
88
-
-
0018506624
-
Boundary-Layer Transition. Experiments on Sharp, Slender Cones in Supersonic Free Flight
-
Aug, doi:10.2514/3.61231
-
Reda, D. C., "Boundary-Layer Transition. Experiments on Sharp, Slender Cones in Supersonic Free Flight," AIAA Journal, Vol. 17, No. 8, Aug. 1979, pp. 803-810. doi:10.2514/3.61231
-
(1979)
AIAA Journal
, vol.17
, Issue.8
, pp. 803-810
-
-
Reda, D.C.1
-
89
-
-
0018915350
-
-
Reda, D. C., Comparative Transition Performance of Several Nosetip Materials at Defined by Ballistics-Range Testing, ISA Transactions, 19, No. 1, Jan. 1980, pp. 83-98; also Proceedings of the 25th International Instrumentation Symposium, Instrument Society of America, Pittsburgh, PA, May 1979, pp. 89-104.
-
Reda, D. C., "Comparative Transition Performance of Several Nosetip Materials at Defined by Ballistics-Range Testing," ISA Transactions, Vol. 19, No. 1, Jan. 1980, pp. 83-98; also Proceedings of the 25th International Instrumentation Symposium, Instrument Society of America, Pittsburgh, PA, May 1979, pp. 89-104.
-
-
-
-
90
-
-
57549097269
-
Boundary Layer Transition on Blunt Axisymmetric Nosetips Induced by Single and Multiple Craters
-
AIAA Paper 81-1087, June
-
Todisco, A., Reeves, B., Siegelman, D., and Mascola, R., "Boundary Layer Transition on Blunt Axisymmetric Nosetips Induced by Single and Multiple Craters," AIAA Paper 81-1087, June 1981.
-
(1981)
-
-
Todisco, A.1
Reeves, B.2
Siegelman, D.3
Mascola, R.4
-
91
-
-
0021196772
-
-
AIAA Paper 84-0631, Mar
-
Wassel, A. T., Shih, W. C. L., and Courtney, J. F., "Roughness Induced Transition and Heat Transfer Augmentation in Hypersonic Environments," AIAA Paper 84-0631, Mar. 1984.
-
(1984)
Roughness Induced Transition and Heat Transfer Augmentation in Hypersonic Environments
-
-
Wassel, A.T.1
Shih, W.C.L.2
Courtney, J.F.3
-
92
-
-
78149448365
-
Thermal Imaging on Missiles in Hypersonic Flow
-
France, Apr
-
Schöler, H., "Thermal Imaging on Missiles in Hypersonic Flow," Missile Aerodynamics, AGARD CP-493, Neuilly-sur-Seine, France, Apr. 1990, p. 29.
-
(1990)
Missile Aerodynamics, AGARD CP-493, Neuilly-sur-Seine
, pp. 29
-
-
Schöler, H.1
-
93
-
-
0022944632
-
-
Holden, M. S., Studies of Potential Fluid-Mechanical Mechanisms for Enhanced Stagnation-Point Heating, Thermophysical Aspects of Reentry Flows, edited by J. N. Moss and C. D. Scott, 103, Progress in Astronautics and Aeronautics, AIAA, New York, 1986, pp. 281-309.
-
Holden, M. S., "Studies of Potential Fluid-Mechanical Mechanisms for Enhanced Stagnation-Point Heating," Thermophysical Aspects of Reentry Flows, edited by J. N. Moss and C. D. Scott, Vol. 103, Progress in Astronautics and Aeronautics, AIAA, New York, 1986, pp. 281-309.
-
-
-
-
94
-
-
57549087018
-
-
Holden, M. S., and Rodriguez, K. M., Studies of Shock/Shock Interaction on Smooth and Transpiration-Cooled Hemispherical Nosetips In Hypersonic Flows, NASA, CR-189585, Apr. 1992; also Calspan Advanced Technology Center, TR 7931, Buffalo, NY, Apr. 1992.
-
Holden, M. S., and Rodriguez, K. M., "Studies of Shock/Shock Interaction on Smooth and Transpiration-Cooled Hemispherical Nosetips In Hypersonic Flows," NASA, CR-189585, Apr. 1992; also Calspan Advanced Technology Center, TR 7931, Buffalo, NY, Apr. 1992.
-
-
-
-
95
-
-
4243138593
-
Laminar Turbulent Transition at Hypersonic Speeds: The Effects of Nose Blunting
-
ESA, Paris, Feb. 1.995, pp
-
Zanchetta, M. A., and Hillier, R., "Laminar Turbulent Transition at Hypersonic Speeds: The Effects of Nose Blunting," 2nd European Symposium on Aerotliermodynamics for Space Vehicles, ESA, Paris, Feb. 1.995, pp. 207-212.
-
2nd European Symposium on Aerotliermodynamics for Space Vehicles
, pp. 207-212
-
-
Zanchetta, M.A.1
Hillier, R.2
-
96
-
-
0642335215
-
Kinetic heating and transition studies at hypersonic speeds,
-
Ph.D. Thesis, Dept. of Aeronautics, Imperial College of Science, Technology, and Medicine, London, Apr
-
Zanchetta, M., "Kinetic heating and transition studies at hypersonic speeds," Ph.D. Thesis, Dept. of Aeronautics, Imperial College of Science, Technology, and Medicine, London, Apr. 1996.
-
(1996)
-
-
Zanchetta, M.1
-
97
-
-
57549102770
-
Hypersonic Aerothermodynamics at VKI
-
France, Oct
-
Carbonaro, M., Charbonnier, J.-M., and Deconinck, H., "Hypersonic Aerothermodynamics at VKI," Aerothermodynamlcs and Propulsion Integration for Hypersonic Vehicles, AGARD, R-813, Neuilly-surSeine, France, Oct. 1996.
-
(1996)
Aerothermodynamlcs and Propulsion Integration for Hypersonic Vehicles, AGARD, R-813, Neuilly-surSeine
-
-
Carbonaro, M.1
Charbonnier, J.-M.2
Deconinck, H.3
-
98
-
-
57549104347
-
Roughness-Induced Transition in Hypersonic Flow
-
Mar
-
Charbonnier, J.-M., and Boerrigter, H., "Roughness-Induced Transition in Hypersonic Flow," Space Scientific Research in Belgium," Vol. 4, Mar. 1996, pp. 43-44.
-
(1996)
Space Scientific Research in Belgium
, vol.4
, pp. 43-44
-
-
Charbonnier, J.-M.1
Boerrigter, H.2
-
99
-
-
57549105462
-
Roughness-Induced Transition in Hypersonic Flow
-
Mar
-
Boerrigter, H., and Charbonnier, J.-M., "Roughness-Induced Transition in Hypersonic Flow," Space Scientific Research in Belgium," Vol. 4, Mar. 1996, pp. 51-52.
-
(1996)
Space Scientific Research in Belgium
, vol.4
, pp. 51-52
-
-
Boerrigter, H.1
Charbonnier, J.-M.2
-
100
-
-
0031188570
-
Effects of Isolated Roughness Elements on Boundary-Layer Transition for Shuttle Orbiter
-
July-Aug, doi:10.2514/2.3254
-
Bertin, J. J., Stetson, K. F., Bouslog, S. A., and Caram, J. M., "Effects of Isolated Roughness Elements on Boundary-Layer Transition for Shuttle Orbiter," Journal of Spacecraft and Rockets, Vol. 34, No. 4, July-Aug. 1997, pp. 426-436. doi:10.2514/2.3254
-
(1997)
Journal of Spacecraft and Rockets
, vol.34
, Issue.4
, pp. 426-436
-
-
Bertin, J.J.1
Stetson, K.F.2
Bouslog, S.A.3
Caram, J.M.4
-
101
-
-
57549089240
-
Simulation of Transitional and Turbulent Boundary Layer Flow on Blunted Geometry in Hypersonic Flow
-
ESA, Paris, Nov
-
Charbonnier, J.-M., Dieudonne, W., and Boerrigter, H., "Simulation of Transitional and Turbulent Boundary Layer Flow on Blunted Geometry in Hypersonic Flow," 3rd European Symposium on Aerothermodynamics for Space Vehicles, ESA, Paris, Nov. 1998, pp. 291-297.
-
(1998)
3rd European Symposium on Aerothermodynamics for Space Vehicles
, pp. 291-297
-
-
Charbonnier, J.-M.1
Dieudonne, W.2
Boerrigter, H.3
-
102
-
-
57549106227
-
Roughness-Induced Transition for Flight Experiments
-
CD-ROM, Association Aéronautique et Astronautique de France, Paris, Mar
-
Paris, S., Fletcher, D., Cerignat, L., and Garzon, A., "Roughness-Induced Transition for Flight Experiments," Fourth International Symposium on Atmospheric Reentry Vehicles and Systems [CD-ROM], Association Aéronautique et Astronautique de France, Paris, Mar. 2005.
-
(2005)
Fourth International Symposium on Atmospheric Reentry Vehicles and Systems
-
-
Paris, S.1
Fletcher, D.2
Cerignat, L.3
Garzon, A.4
-
103
-
-
0343036075
-
Blunt Body Near-Wake Flow Field at Mach 6
-
AIAA Paper 96-1935, June
-
Horvath, T. J., McGinley, C. B., and Hannemann, K., "Blunt Body Near-Wake Flow Field at Mach 6, AIAA Paper 96-1935, June 1996.
-
(1996)
-
-
Horvath, T.J.1
McGinley, C.B.2
Hannemann, K.3
-
104
-
-
84894548756
-
Aerothermodynamic Environment Definition for the Genesis Sample Return Capsule
-
AIAA Paper 2001-2889, June
-
Cheatwood, F. M., Merski, N. R., Riley, C. J., and Mitcheltree, R. A., "Aerothermodynamic Environment Definition for the Genesis Sample Return Capsule," AIAA Paper 2001-2889, June 2001.
-
(2001)
-
-
Cheatwood, F.M.1
Merski, N.R.2
Riley, C.J.3
Mitcheltree, R.A.4
-
105
-
-
34347237592
-
Analysis of the Forebody Aeroheating Environment During Genesis Sample Return Capsule Reentry
-
AIAA Paper 2007-1207, Jan
-
Tang, Chun Y., and Wright, M. J., "Analysis of the Forebody Aeroheating Environment During Genesis Sample Return Capsule Reentry," AIAA Paper 2007-1207, Jan. 2007.
-
(2007)
-
-
Tang, C.Y.1
Wright, M.J.2
-
106
-
-
85085776099
-
Boundary-Layer Transition Correlations and Aeroheating Predictions for Mars Smart Lander
-
June
-
Hollis, B. R., and Liechty, D. S., "Boundary-Layer Transition Correlations and Aeroheating Predictions for Mars Smart Lander," AIAA, Paper 2002-2745, June 2002.
-
(2002)
AIAA, Paper 2002-2745
-
-
Hollis, B.R.1
Liechty, D.S.2
-
107
-
-
33646708960
-
-
Edquist, Karl T., Liechty, Derek S., Hollis, B. R., Alter, S. J., and Loomis, M. P., Aeroheating Environments for a Mars Smart Lander, Journal of Spacecraft and Rockets, 43, No. 2, Mar.-Apr. 2006, pp. 330-339. doi:10.2514/1.19431
-
Edquist, Karl T., Liechty, Derek S., Hollis, B. R., Alter, S. J., and Loomis, M. P., "Aeroheating Environments for a Mars Smart Lander," Journal of Spacecraft and Rockets, Vol. 43, No. 2, Mar.-Apr. 2006, pp. 330-339. doi:10.2514/1.19431
-
-
-
-
108
-
-
34347240752
-
Aerothermodynamic Environments Definition for the Mars Science Laboratory Entry Capsule
-
Jan
-
Edquist, K. T., Dyakonov, A. A., Wright, M. J., and Tang, C. Y., "Aerothermodynamic Environments Definition for the Mars Science Laboratory Entry Capsule," AIAA, Paper 2007-1206, Jan. 2007.
-
(2007)
AIAA, Paper
, vol.2007 -1206
-
-
Edquist, K.T.1
Dyakonov, A.A.2
Wright, M.J.3
Tang, C.Y.4
-
109
-
-
34347217848
-
-
AIAA, Paper 2007-1208, Jan
-
Hollis, B. R., and Collier, A. S., 'Turbulent Aeroheating Testing of Mars Science Laboratory Entry Vehicle in Perfect-Gas Nitrogen," AIAA, Paper 2007-1208, Jan. 2007.
-
(2007)
Turbulent Aeroheating Testing of Mars Science Laboratory Entry Vehicle in Perfect-Gas Nitrogen
-
-
Hollis, B.R.1
Collier, A.S.2
-
110
-
-
57349136163
-
Measurements of Fluctuating Pitot Pressure, 'Tunnel Noise' in the AEDC Hypervelocity Wind Tunnel No. 9
-
AIAA Paper 2007-1678, Feb
-
Lafferty, J. F., and Norris, J. D., "Measurements of Fluctuating Pitot Pressure, 'Tunnel Noise' in the AEDC Hypervelocity Wind Tunnel No. 9," AIAA Paper 2007-1678, Feb. 2007.
-
(2007)
-
-
Lafferty, J.F.1
Norris, J.D.2
-
111
-
-
23844446274
-
Experiments on Hypersonic Roughness Induced Transition by Means of Infrared Thermography
-
ESA, Paris, Nov
-
Schrijer, F. F. J., Scarano, F., Van Oudheusden, B. W., and Bannink, W. J., "Experiments on Hypersonic Roughness Induced Transition by Means of Infrared Thermography," 5th European Symposium on Aerothermodynamics for Space Vehicles, ESA, Paris, Nov. 2004, pp. 255-260.
-
(2004)
5th European Symposium on Aerothermodynamics for Space Vehicles
, pp. 255-260
-
-
Schrijer, F.F.J.1
Scarano, F.2
Van Oudheusden, B.W.3
Bannink, W.J.4
-
112
-
-
57549103980
-
Aerothermodynamic Testing of Ablative Reentry Vehicle Nosetip Materials in Hypersonic Ballistic-Range Environments
-
Nov
-
Reda, D. C., Wilder, M. C., Bogdanoff, D. W., and Glejniczak, J., "Aerothermodynamic Testing of Ablative Reentry Vehicle Nosetip Materials in Hypersonic Ballistic-Range Environments," AIAA, Paper 2004-6829, Nov. 2004.
-
(2004)
AIAA, Paper 2004-6829
-
-
Reda, D.C.1
Wilder, M.C.2
Bogdanoff, D.W.3
Glejniczak, J.4
-
113
-
-
34250803939
-
-
AIAA Paper 2007-0306, Jan
-
Reda, D. C., Wilder, M. C., Bogdanoff, D. W., and Prabhu, D., "Transition Experiments on Blunt Bodies with Distributed Roughness in Hypersonic Free Flight," AIAA Paper 2007-0306, Jan. 2007.
-
(2007)
Transition Experiments on Blunt Bodies with Distributed Roughness in Hypersonic Free Flight
-
-
Reda, D.C.1
Wilder, M.C.2
Bogdanoff, D.W.3
Prabhu, D.4
-
114
-
-
34347250793
-
Testing of the Crew Exploration Vehicle in NASA Langley's Unitary Plan Wind Tunnel
-
AIAA Paper 2007-1005, Jan
-
Murphy, K. J., Borg, S. E., Watkins, A. N., Cole, D. R., and Schwartz, R. J., "Testing of the Crew Exploration Vehicle in NASA Langley's Unitary Plan Wind Tunnel," AIAA Paper 2007-1005, Jan. 2007.
-
(2007)
-
-
Murphy, K.J.1
Borg, S.E.2
Watkins, A.N.3
Cole, D.R.4
Schwartz, R.J.5
-
115
-
-
3242833951
-
-
NASA TN, Sept
-
Braslow, A. L., Hicks, R. M., and Harris, R. V., Jr., "Use of Grit-Type Boundary-Layer Transition Trips on Wind-Tunnel Models," NASA TN-D-3579, Sept. 1966.
-
(1966)
Use of Grit-Type Boundary-Layer Transition Trips on Wind-Tunnel Models
-
-
Braslow, A.L.1
Hicks, R.M.2
Harris Jr., R.V.3
-
116
-
-
34250805907
-
Aerodynamic Testing in Support of Orion Spacecraft Development
-
AIAA Paper 2007-1004, Jan
-
Ross, J. C., "Aerodynamic Testing in Support of Orion Spacecraft Development," AIAA Paper 2007-1004, Jan. 2007.
-
(2007)
-
-
Ross, J.C.1
-
117
-
-
57549083240
-
Free-Flight Measurements of Static and Dynamic Stability of Models of the Project Mercury Re-Entry Capsule at Mach Numbers 3 and 9.5
-
NASA TM-X-373, Aug
-
Sommer, S. C., Short, B. J., and Compton, D. L., "Free-Flight Measurements of Static and Dynamic Stability of Models of the Project Mercury Re-Entry Capsule at Mach Numbers 3 and 9.5," NASA TM-X-373, Aug. 1960.
-
(1960)
-
-
Sommer, S.C.1
Short, B.J.2
Compton, D.L.3
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