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Volumn 45, Issue 6, 2008, Pages 1090-1105

Summary of hypersonic boundary-layer transition experiments on blunt bodies with roughness

Author keywords

[No Author keywords available]

Indexed keywords

AUTOMOBILE BODIES; HYPERSONIC FLOW; HYPERSONIC VEHICLES;

EID: 57549109669     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.37431     Document Type: Article
Times cited : (85)

References (117)
  • 2
    • 57549109455 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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
  • 7
    • 0035332207 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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.
  • 27
    • 57549118903 scopus 로고
    • 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 scopus 로고
    • 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
  • 34
    • 33846093617 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고
    • 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
  • 42
    • 57549098407 scopus 로고
    • 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
  • 44
    • 57549091777 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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.
  • 63
    • 85003324745 scopus 로고
    • 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 scopus 로고
    • 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
  • 66
    • 57549111845 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 61, NASA TN-D-391, July 1960.
    • 61," NASA TN-D-391, July 1960.
  • 76
    • 57549095004 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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
  • 79
    • 85007721154 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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.
  • 82
    • 57549108673 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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
  • 87
    • 57549112555 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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
  • 93
    • 0022944632 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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.
  • 96
    • 0642335215 scopus 로고    scopus 로고
    • 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
  • 100
    • 0031188570 scopus 로고    scopus 로고
    • 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
  • 103
    • 0343036075 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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
  • 110
    • 57349136163 scopus 로고    scopus 로고
    • 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
  • 112
    • 57549103980 scopus 로고    scopus 로고
    • 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
  • 114
    • 34347250793 scopus 로고    scopus 로고
    • 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
  • 116
    • 34250805907 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.