-
2
-
-
84897713998
-
-
AIAA -2002-5259, Sept.
-
Hale, N. W., Lamotte, N. O., and Garner, T. W., "Operational Experience with Hypersonic flight of the Space Shuttle," AIAA -2002-5259, Sept., 2002.
-
(2002)
Operational Experience with Hypersonic Flight of the Space Shuttle
-
-
Hale, N.W.1
Lamotte, N.O.2
Garner, T.W.3
-
3
-
-
0002859427
-
Orbiter windward surface boundary layer transition flight data
-
NASA CP-3248, April
-
Bouslog, S. A., An, M. Y., and Derry, S. M., "Orbiter Windward Surface Boundary Layer Transition Flight Data," NASA CP-3248, Orbiter Experiments (OEX) Aerothermodynamics Symposium, April 1995, pp. 703-739.
-
(1995)
Orbiter Experiments (OEX) Aerothermodynamics Symposium
, pp. 703-739
-
-
Bouslog, S.A.1
An, M.Y.2
Derry, S.M.3
-
4
-
-
0020906412
-
Shuttle orbiter boundary layer transition at flight and wind tunnel conditions
-
NASA CP 2283, March
-
Goodrich, W. D., Derry, S. M., and Bertin, J. J., "Shuttle Orbiter Boundary Layer Transition at Flight and Wind Tunnel Conditions," Shuttle Performance: Lessons Learned, Part 2, NASA CP 2283, March 1983, pp. 753-779.
-
(1983)
Shuttle Performance: Lessons Learned, Part 2
, pp. 753-779
-
-
Goodrich, W.D.1
Derry, S.M.2
Bertin, J.J.3
-
5
-
-
33845584340
-
-
AIAA-2006-2917, June
-
Campbell, C. H., Anderson, B., Bourland, G., Bouslog, S., Cassady, A., Horvath, T., Berry, S., Gnoffo, P., Wood, B., Reuther, J., Driver, D., Chao, D., and Picetti, D., "Orbiter Return To Flight Entry Aeroheating," AIAA-2006-2917, June 2006.
-
(2006)
Orbiter Return to Flight Entry Aeroheating
-
-
Campbell, C.H.1
Anderson, B.2
Bourland, G.3
Bouslog, S.4
Cassady, A.5
Horvath, T.6
Berry, S.7
Gnoffo, P.8
Wood, B.9
Reuther, J.10
Driver, D.11
Chao, D.12
Picetti, D.13
-
6
-
-
33845571449
-
-
AIAA-2006-2918, June
-
Berry, S. A., Horvath, T. J., Greene, F. A., Kinder, G. R., and Wang, K. C., "Overview of Boundary Layer Transition Research in Support of Orbiter Return To Flight," AIAA-2006-2918, June 2006.
-
(2006)
Overview of Boundary Layer Transition Research in Support of Orbiter Return to Flight
-
-
Berry, S.A.1
Horvath, T.J.2
Greene, F.A.3
Kinder, G.R.4
Wang, K.C.5
-
8
-
-
33845525581
-
-
AIAA-2006-2921, June
-
McGinley, C., Berry, S. A., Kinder, G. R., Barnwell, M., Wang, K. C., and Kirk, B. S., "Review of Orbiter Flight Boundary Layer Transition Data," AIAA-2006-2921, June 2006.
-
(2006)
Review of Orbiter Flight Boundary Layer Transition Data
-
-
McGinley, C.1
Berry, S.A.2
Kinder, G.R.3
Barnwell, M.4
Wang, K.C.5
Kirk, B.S.6
-
9
-
-
33845595923
-
-
AIAA-2006-2922, June
-
Berry, S. A., Horvath, T. J., Cassady, M. A., Kirk, B. S., Wang, K.C., and Hyatt, A. J., "Boundary Layer Transition Results From STS-114," AIAA-2006-2922, June 2006.
-
(2006)
Boundary Layer Transition Results from STS-114
-
-
Berry, S.A.1
Horvath, T.J.2
Cassady, M.A.3
Kirk, B.S.4
Wang, K.C.5
Hyatt, A.J.6
-
10
-
-
85086615500
-
Discrete roughness effects on shuttle orbiter at Mach 6
-
June
-
Berry, S. A., and Hamilton, H. H., "Discrete Roughness Effects on Shuttle Orbiter at Mach 6," AIAA Paper 2002-2744, June. 2002.
-
(2002)
AIAA Paper
, vol.2002
, Issue.2744
-
-
Berry, S.A.1
Hamilton, H.H.2
-
11
-
-
0032075307
-
Shuttle orbiter experimental boundary-layer transition results with isolated roughness
-
Berry, S. A., Bouslog, S. A., Brauckmann, G. J., and Caram, J. M., "Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness," Journal of Spacecraft and Rockets, Vol. 35, No. 3, 1998, pp. 241-248.
-
(1998)
Journal of Spacecraft and Rockets
, vol.35
, Issue.3
, pp. 241-248
-
-
Berry, S.A.1
Bouslog, S.A.2
Brauckmann, G.J.3
Caram, J.M.4
-
12
-
-
33748040335
-
-
NASA Johnson Space Center, JSC-26812, Oct.
-
Bouslog, S. A., An, M. Y., Campbell, C. H., Wang, K. C., and Pelley, R. L., "Orbiter Boundary-Layer Transition Working Group: Analysis and Ground Test Status Report," NASA Johnson Space Center, JSC-26812, Oct. 1994.
-
(1994)
Orbiter Boundary-layer Transition Working Group: Analysis and Ground Test Status Report
-
-
Bouslog, S.A.1
An, M.Y.2
Campbell, C.H.3
Wang, K.C.4
Pelley, R.L.5
-
13
-
-
0020543185
-
A review of roughness-induced nosetip transition
-
Jan.
-
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.
-
(1983)
AIAA Journal
, vol.21
, Issue.1
, pp. 7-22
-
-
Batt, R.G.1
Legner, H.H.2
-
14
-
-
0002730529
-
Boundary layer transition on cones and spheres at supersonic speeds -effects of roughness and cooling
-
July
-
Van Driest, E. R., and Blummer, 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, Report 67-2048, July 1967.
-
(1967)
U.S. Air Force Office of Scientific Research, Report
, vol.67
, Issue.2048
-
-
Van Driest, E.R.1
Blummer, C.B.2
-
15
-
-
84983167052
-
Boundary layer transition flight test observations
-
Jan.
-
Berkowitz, A. M., Kyriss, C. L., and Martellucci, A., "Boundary Layer Transition Flight Test Observations," AIAA Paper 77-125, Jan. 1977.
-
(1977)
AIAA Paper
, vol.77
, Issue.125
-
-
Berkowitz, A.M.1
Kyriss, C.L.2
Martellucci, A.3
-
16
-
-
0018491364
-
Artificially induced boundary-layer transition on blunt-slender cones at hypersonic speeds
-
Boudreau, A. H., "Artificially Induced Boundary-Layer Transition on Blunt-Slender Cones at Hypersonic Speeds," Journal of Spacecraft and Rockets, Vol. 16, No. 4, 1979, pp. 245-251.
-
(1979)
Journal of Spacecraft and Rockets
, vol.16
, Issue.4
, pp. 245-251
-
-
Boudreau, A.H.1
-
17
-
-
0004731234
-
-
Arnold Engineering Development Center, TR-77-107, Arnold Air Force Station, TN, March
-
Pate, S. R., "Dominance of Radiated Aerodynamic Noise on Boundary-Layer Transition in Supersonic-Hypersonic Wind Tunnels," Arnold Engineering Development Center, TR-77-107, Arnold Air Force Station, TN, March 1978.
-
(1978)
Dominance of Radiated Aerodynamic Noise on Boundary-layer Transition in Supersonic-hypersonic Wind Tunnels
-
-
Pate, S.R.1
-
18
-
-
33748075046
-
The effect of transition and boundary layer development on hypersonic reentry shape change
-
May
-
Dirling, R. B. Jr., Swain, C. E., and Stokes, T. R., "The Effect of Transition and Boundary Layer Development on Hypersonic Reentry Shape Change," AIAA Paper 75-673, May 1975.
-
(1975)
AIAA Paper
, vol.75
, Issue.673
-
-
Dirling Jr., R.B.1
Swain, C.E.2
Stokes, T.R.3
-
20
-
-
0036493808
-
Review and synthesis of roughness-dominated transition correlations for reentry applications
-
Reda, D. C., "Review and Synthesis of roughness-Dominated Transition Correlations for Reentry Applications," Journal of Spacecraft and Rockets, Vol. 39, No. 2, pp. 161-167.
-
Journal of Spacecraft and Rockets
, vol.39
, Issue.2
, pp. 161-167
-
-
Reda, D.C.1
-
21
-
-
0020906412
-
Shuttle boundary layer transition at flight and wind tunnel conditions
-
NASA CP 2283, March
-
Goodrich, W. D., Derry, S. M., and Bertin, J. J., "Shuttle Boundary Layer Transition at Flight and Wind Tunnel Conditions," Shuttle Performance: Lessons Learned, Part 2, NASA CP 2283, March, 1983, pp. 753-779.
-
(1983)
Shuttle Performance: Lessons Learned, Part 2
, pp. 753-779
-
-
Goodrich, W.D.1
Derry, S.M.2
Bertin, J.J.3
-
22
-
-
0001325343
-
An investigation of separated flows-part I: The pressure field
-
June
-
Charwat, A. F., Roos, J. N., Dewey, C. F., Jr., and Hitz, J. A., "An Investigation of Separated Flows-Part I: The Pressure Field," Journal of Aerospace Sciences, Vol. 28, No. 6, June 1961, pp. 457-470.
-
(1961)
Journal of Aerospace Sciences
, vol.28
, Issue.6
, pp. 457-470
-
-
Charwat, A.F.1
Roos, J.N.2
Dewey Jr., C.F.3
Hitz, J.A.4
-
23
-
-
0001325343
-
An investigation of separated flows-part II: Flow in the cavity and heat transfer
-
July
-
Charwat, A. F., Dewey, C. F., Roos, J. N., Jr., and Hitz, J. A., "An Investigation of Separated Flows-Part II: Flow in the Cavity and Heat Transfer," Journal of Aerospace Sciences, Vol. 28, No. 7, July 1961, pp. 513-527.
-
(1961)
Journal of Aerospace Sciences
, vol.28
, Issue.7
, pp. 513-527
-
-
Charwat, A.F.1
Dewey, C.F.2
Roos Jr., J.N.3
Hitz, J.A.4
-
24
-
-
0021873741
-
The effects of surface discontinuities on convective heat transfer in hypersonic flow
-
June
-
Nestler, D. E., "The Effects of Surface Discontinuities on Convective Heat Transfer in Hypersonic Flow," AIAA Paper 85-0971, June. 1985.
-
(1985)
AIAA Paper
, vol.85
, Issue.971
-
-
Nestler, D.E.1
-
25
-
-
33845575200
-
Cone cavity flow at Mach 5.3 with injection of light, medium, and heavy gas
-
Technical Report VKI TN 35, Von Karman Institute for Fluid Dynamics, November. DTIC Citation AD681533
-
Ginoux, J. J, Thiry, F., "Cone Cavity Flow at Mach 5.3 with Injection of Light, Medium, and Heavy Gas," Technical Report VKI TN 35, AFOSR Final Report 69-0618, Von Karman Institute for Fluid Dynamics, November, 1968. DTIC Citation AD681533.
-
(1968)
AFOSR Final Report
, vol.69
, Issue.618
-
-
Ginoux, J.J.1
Thiry, F.2
-
26
-
-
33845585213
-
Laminar separation in supersonic and hypersonic flows
-
Technical Report VKI TN 35, Von Karman Institute for Fluid Dynamics, September. DTIC Citation AD6647819
-
Ginoux, J. J, "Laminar Separation in Supersonic and Hypersonic Flows," Technical Report VKI TN 35, AFOSR Final Report 67-0615, Von Karman Institute for Fluid Dynamics, September, 1966. DTIC Citation AD6647819.
-
(1966)
AFOSR Final Report
, vol.67
, Issue.615
-
-
Ginoux, J.J.1
-
29
-
-
0007619937
-
-
Technical Report NASA TN-D-349, NASA, December
-
Larson, H. K., and Keating, S. J., Jr. "Transition Reynolds Numbers of Separated Flows at Supersonic Speeds," Technical Report NASA TN-D-349, NASA, December 1960.
-
(1960)
Transition Reynolds Numbers of Separated Flows at Supersonic Speeds
-
-
Larson, H.K.1
Keating Jr., S.J.2
-
30
-
-
0026185813
-
Experimental transition investigation of a free-shear layer above a cavity at Mach 3.5
-
King, R. A., Creel, T. R. Jr., and Bushnell, D. M., "Experimental Transition Investigation of a Free-Shear Layer Above a Cavity at Mach 3.5," Journal of Propulsion, 1991, pp. 626-634.
-
(1991)
Journal of Propulsion
, pp. 626-634
-
-
King, R.A.1
Creel Jr., T.R.2
Bushnell, D.M.3
-
31
-
-
33845574125
-
Experimental investigation of separated flow qver a cavity at hypersonic speed
-
June
-
Hahn, M., "Experimental Investigation of Separated Flow Qver a Cavity at Hypersonic Speed," AIAA Paper 68-672, June 1968.
-
(1968)
AIAA Paper
, vol.68
, Issue.672
-
-
Hahn, M.1
-
32
-
-
85007692135
-
Effect of mass injection into a cavity on hypersonic boundary-layer transition
-
August
-
Morrisette, L. E., Effect of Mass Injection Into a Cavity on Hypersonic Boundary-Layer Transition." AIAA Journal, Vol. 4. No. 8, August 1966, pp. 1488-1489.
-
(1966)
AIAA Journal
, vol.4
, Issue.8
, pp. 1488-1489
-
-
Morrisette, L.E.1
-
33
-
-
85088182181
-
Assessment of LAURA for laminar supersonic shallow cavities
-
June
-
Wood, W. A., Pulsonetti, M.V., Everhart, J.L., and Bey, K.S., "Assessment of LAURA for Laminar Supersonic Shallow Cavities. AIAA Paper 2004-2639, June 2004.
-
(2004)
AIAA Paper
, vol.2004
, Issue.2639
-
-
Wood, W.A.1
Pulsonetti, M.V.2
Everhart, J.L.3
Bey, K.S.4
-
34
-
-
84894548756
-
Aerothermodynamic environment definition for the genesis sample return capsule
-
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)
AIAA Paper
, vol.2001
, Issue.2889
-
-
Cheatwood, F.M.1
Merski, N.R.2
Riley, C.J.3
Mitcheltree, R.A.4
-
35
-
-
85088182181
-
Assessment of LAURA for laminar supersonic shallow cavities
-
June
-
Wood, W. A., Pulsonetti, M.V., Everhart, J.L., and Bey, K.S., "Assessment of LAURA for Laminar Supersonic Shallow Cavities. AIAA Paper 2004-2639, June 2004.
-
(2004)
AIAA Paper
, vol.2004
, Issue.2639
-
-
Wood, W.A.1
Pulsonetti, M.V.2
Everhart, J.L.3
Bey, K.S.4
-
36
-
-
85085776099
-
Boundary-layer transition correlations and aeroheating predictions for mars smart lander
-
June
-
Hollis, B.R., Liechty, D.S., "Boundary-Layer Transition Correlations and Aeroheating Predictions for Mars Smart Lander," AIAA Paper 2002-2745, June 2002.
-
(2002)
AIAA Paper
, vol.2002
, Issue.2745
-
-
Hollis, B.R.1
Liechty, D.S.2
-
37
-
-
33845594283
-
-
Technical Report NASA-CR-1908, December
-
Stalmach, C. J., Jr., Bertin, J.J., Pope, T.C., and McCloskey, M.H., "A Study of Boundary Layer Transition on Outgassing Cones in Hypersonic Flow," Technical Report NASA-CR-1908, December 1971.
-
(1971)
A Study of Boundary Layer Transition on Outgassing Cones in Hypersonic Flow
-
-
Stalmach Jr., C.J.1
Bertin, J.J.2
Pope, T.C.3
McCloskey, M.H.4
-
38
-
-
78049525963
-
Exploratory heat-transfer measurements at Mach 10 on a 7.5-deg. Total-angle cone downstream of a region of air and helium transpiration cooling
-
December
-
Dunavant, J. C., and Everhart, P. E., "Exploratory Heat-Transfer Measurements at Mach 10 on a 7.5-deg. Total-Angle Cone Downstream of a Region of Air and Helium Transpiration Cooling," NASA Technical Note TN-D-5554, December 1969.
-
(1969)
NASA Technical Note
, vol.TN-D-5554
-
-
Dunavant, J.C.1
Everhart, P.E.2
-
39
-
-
0042739513
-
Development of the U.S. Air Force intercontinental ballistic missile weapon systems
-
July-August
-
Lin, T.C., "Development of the U.S. Air Force Intercontinental Ballistic Missile Weapon Systems. Journal of Spacecraft and Rockets, Vol. 40, No. 4, July-August 2003, pp. 491-509.
-
(2003)
Journal of Spacecraft and Rockets
, vol.40
, Issue.4
, pp. 491-509
-
-
Lin, T.C.1
-
40
-
-
0020968575
-
Galileo probe forebody flow-field predictions, "entry vehicle heating and thermal protection system: Space shuttle, solar star probe, galileo probe,"
-
ed. PE Eaver, HE Collicoft
-
Moss, J. N., and Simmonds, A. L., "Galileo Probe Forebody Flow-field Predictions, "Entry Vehicle Heating and Thermal Protection System: Space Shuttle, Solar Star Probe, Galileo Probe," Progress in Astronautics and Aeronautics, ed. PE Eaver, HE Collicoft, Vol. 85, pp. 419-445, 1983.
-
(1983)
Progress in Astronautics and Aeronautics
, vol.85
, pp. 419-445
-
-
Moss, J.N.1
Simmonds, A.L.2
-
41
-
-
84896693583
-
Boundary layer control for hypersonic airbreathing vehicles
-
June
-
Berry, S. A., Nowak, R, J., and Horvath, T. J., "Boundary Layer Control for Hypersonic Airbreathing Vehicles," AIAA Paper 2004-2246, June, 2004.
-
(2004)
AIAA Paper
, vol.2004
, Issue.2246
-
-
Berry, S.A.1
Nowak, R.J.2
Horvath, T.J.3
-
42
-
-
33845589567
-
Fabrication of 0.0075-scale orbiter phosphor thermography test models for shuttle RTF aeroheating studies
-
May
-
Buck, G. M., Powers, M. A., Griffith, M. S., Hopkins, J. W., Veneris, P. H., and Kuykendoll, K. A., "Fabrication of 0.0075-Scale Orbiter Phosphor Thermography Test Models for Shuttle RTF Aeroheating Studies," NASA TM-2006-214303, May 2006.
-
(2006)
NASA TM-2006-214303
-
-
Buck, G.M.1
Powers, M.A.2
Griffith, M.S.3
Hopkins, J.W.4
Veneris, P.H.5
Kuykendoll, K.A.6
-
43
-
-
0002824511
-
Langley hypersonic aerodynamic/aerothermodynamic testing capabilities - Present and future
-
June
-
Miller, C. G., "Langley Hypersonic Aerodynamic/Aerothermodynamic Testing Capabilities - Present and Future," AIAA Paper 90-1376, June 1990.
-
(1990)
AIAA Paper
, vol.90
, Issue.1376
-
-
Miller, C.G.1
-
44
-
-
84896693468
-
Comparison between a hybrid constant-current anemometer and constant-voltage anemometer in hypersonic flow
-
June
-
Chokani, N., Shipluk, A. N., Sidorenko, A. A., and McGinley, C. B.,"Comparison Between a Hybrid Constant-Current Anemometer and Constant-Voltage Anemometer in Hypersonic Flow," AIAA Paper 2004-2248, June, 2004.
-
(2004)
AIAA Paper
, vol.2004
, Issue.2248
-
-
Chokani, N.1
Shipluk, A.N.2
Sidorenko, A.A.3
McGinley, C.B.4
-
46
-
-
0035332207
-
Effects of high-speed tunnel noise on laminar-turbulent transition
-
May-June
-
Schneider, S. P., "Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition," J. of Spacecraft and Rockets, Vol. 38, no. 3, May-June 2001, pp. 323-333
-
(2001)
J. of Spacecraft and Rockets
, vol.38
, Issue.3
, pp. 323-333
-
-
Schneider, S.P.1
-
47
-
-
0005653329
-
Boundary-layer receptivity to transient convected disturbances
-
July
-
Dietz, A. J., "Boundary-Layer Receptivity to Transient Convected Disturbances" AIAA Journal, Vol. 36, No. 7, July, 1998.
-
(1998)
AIAA Journal
, vol.36
, Issue.7
-
-
Dietz, A.J.1
-
48
-
-
2342539427
-
Automated thermal mapping techniques using chromatic image analysis
-
April
-
Buck, G. M., "Automated Thermal Mapping Techniques Using Chromatic Image Analysis," NASA TM 101554, April 1989.
-
(1989)
NASA TM 101554
-
-
Buck, G.M.1
-
49
-
-
84982318636
-
Reduction and analysis of phosphor thermography data with the IHEAT software package
-
Jan.
-
Merski, N. R., "Reduction and Analysis of Phosphor Thermography Data With the IHEAT Software Package," AIAA Paper 98-0712, Jan. 1998.
-
(1998)
AIAA Paper
, vol.98
, Issue.712
-
-
Merski, N.R.1
-
50
-
-
0033100191
-
Global aeroheating wind-tunnel measurements using improved two-color phosphor thermography method
-
Merski, N. R., "Global Aeroheating Wind-Tunnel Measurements Using Improved Two-Color Phosphor Thermography Method" Journal of Spacecraft and Rockets, Vol. 36, No. 2, 1998, pp. 160-170.
-
(1998)
Journal of Spacecraft and Rockets
, vol.36
, Issue.2
, pp. 160-170
-
-
Merski, N.R.1
-
51
-
-
2342507704
-
X-38 experimental aerothermodynamics
-
Horvath, T. J., Berry, S. A., Merski, N. R., and Fitzgerald, S. M., "X-38 Experimental Aerothermodynamics," Journal of Spacecraft and Rockets, Vol. 41, No. 2, 2004, pp. 272-292.
-
(2004)
Journal of Spacecraft and Rockets
, vol.41
, Issue.2
, pp. 272-292
-
-
Horvath, T.J.1
Berry, S.A.2
Merski, N.R.3
Fitzgerald, S.M.4
-
52
-
-
0004337253
-
X-33 experimental aeroheating at Mach 6 using phosphor thermography
-
June
-
Horvath, T. J., Berry, S. A., Hollis, B.R., Liechty, D.S., and Merski, N. R., "X-33 Experimental Aeroheating at Mach 6 Using Phosphor Thermography," AIAA Paper 99-3558, June, 1999.
-
(1999)
AIAA Paper
, vol.99
, Issue.3558
-
-
Horvath, T.J.1
Berry, S.A.2
Hollis, B.R.3
Liechty, D.S.4
Merski, N.R.5
-
53
-
-
85041141206
-
An upwind-biased, point-implicit relaxation algorithm for viscous compressible perfect-gas flows
-
Gnoffo, P. A., "An Upwind-Biased, Point-Implicit Relaxation Algorithm for Viscous Compressible Perfect-Gas Flows," NASA TP-2953, 1990
-
(1990)
NASA TP-2953
-
-
Gnoffo, P.A.1
-
55
-
-
85088001431
-
Boundary layer transition on the windward face of the space shuttle during re-entry
-
June
-
Poll, D. I. A., "Boundary Layer Transition on the windward Face of the Space Shuttle During Re-Entry," AIAA Paper 1985-0899, June, 1985.
-
(1985)
AIAA Paper
, vol.1985
, Issue.899
-
-
Poll, D.I.A.1
-
56
-
-
0035438872
-
X-33 hypersonic boundary layer-transition
-
Berry, S. A., Horvath, T. J., Hollis, B. R., Thompson, R. A., and Hamilton II, H. H., "X-33 Hypersonic Boundary Layer-Transition," Journal of Spacecraft and Rockets, Vol. 38, No. 5, 2001, pp. 646-657.
-
(2001)
Journal of Spacecraft and Rockets
, vol.38
, Issue.5
, pp. 646-657
-
-
Berry, S.A.1
Horvath, T.J.2
Hollis, B.R.3
Thompson, R.A.4
Hamilton II, H.H.5
-
57
-
-
85003349540
-
Spreading of a turbulent disturbance
-
July
-
Fischer, M. C., "Spreading of a Turbulent Disturbance," AIAA Journal, Vol. 10, No. 7, July 1972, pp.957-959.
-
(1972)
AIAA Journal
, vol.10
, Issue.7
, pp. 957-959
-
-
Fischer, M.C.1
-
58
-
-
33845577901
-
Shuttle return to flight experimental results: Protuberance effects on boundary layer transition
-
May
-
Liechty, D. S., Berry, S. A., and Horvath, T. J., "Shuttle Return To flight Experimental Results: Protuberance Effects on Boundary Layer Transition," NASA TM-2006-214306, May 2006.
-
(2006)
NASA TM-2006-214306
-
-
Liechty, D.S.1
Berry, S.A.2
Horvath, T.J.3
-
59
-
-
33845577714
-
Shuttle return to flight experimental results: Cavity effects on boundary layer transition
-
May
-
Liechty, D. S., Horvath, T. J., and Berry, S. A., "Shuttle Return To flight Experimental Results: Cavity Effects on Boundary Layer Transition," NASA TM-2006-214305, May 2006.
-
(2006)
NASA TM-2006-214305
-
-
Liechty, D.S.1
Horvath, T.J.2
Berry, S.A.3
-
60
-
-
2942739133
-
Experimental aerothermodynamics in support of the Columbia accident investigation
-
June
-
Horvath, T. J., "Experimental Aerothermodynamics In Support of the Columbia Accident Investigation," AIAA Paper 2004-1387, June, 2004.
-
(2004)
AIAA Paper
, vol.2004
, Issue.1387
-
-
Horvath, T.J.1
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