-
2
-
-
77958190667
-
-
NASA TM 2006-214528
-
Everhart, Joel L., Berger, Karen T., Bey, Kim S., Merski, N. Ronald, and Wood, William A., "Cavity Heating Experiments Supporting Shuttle Columbia Accident Investigation," NASA TM 2006-214528, 2006.
-
(2006)
Cavity Heating Experiments Supporting Shuttle Columbia Accident Investigation
-
-
Everhart, J.L.1
Berger, K.T.2
Bey, K.S.3
Merski, N.R.4
Wood, W.A.5
-
3
-
-
77958176747
-
-
NASA JSC EG-SS-06-04
-
Everhart, Joel L., Berger, Karen T., Brauckmann, Gregory J, Merski, N. Ronald, and Wood, William A., "Parametric Cavity Heating Experiments Supporting Shuttle Orbiter Return To Flight," NASA JSC EG-SS-06-04, 2007.
-
(2007)
Parametric Cavity Heating Experiments Supporting Shuttle Orbiter Return to Flight
-
-
Everhart, J.L.1
Berger, K.T.2
Brauckmann, G.J.3
Merski, N.R.4
Wood, W.A.5
-
4
-
-
34250894428
-
Pressure gradient effects on hypersonic cavity flow heating
-
AIAA 2006-0185, Presented at, Reno, NV, January 9-12
-
Everhart, Joel L., Alter, Stephen J., Merski, N. Ronald, Wood, William A., and Prabhu, Ramadas K., "Pressure Gradient Effects on Hypersonic Cavity Flow Heating," AIAA 2006-0185, Presented at 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9-12, 2006.
-
(2006)
44th AIAA Aerospace Sciences Meeting and Exhibit
-
-
Everhart, J.L.1
Alter, S.J.2
Merski, N.R.3
Wood, W.A.4
Prabhu, R.K.5
-
5
-
-
77958159774
-
-
NASA JSC EG-SS-06-07
-
Everhart, Joel L., Berger, Karen T., Merski, N. Ronald, Wood, William A., Hollingsworth, Kevin E., Hyatt, Andrew J., and Prabhu, Ramadas K., "Aero-Heating of Shallow Cavities in Hypersonic Freestream Flow," NASA JSC EG-SS-06-07, 2007.
-
(2007)
Aero-Heating of Shallow Cavities in Hypersonic Freestream Flow
-
-
Everhart, J.L.1
Berger, K.T.2
Merski, N.R.3
Wood, W.A.4
Hollingsworth, K.E.5
Hyatt, A.J.6
Prabhu, R.K.7
-
6
-
-
77958176747
-
-
NASA JSC EG-SS-07-01, February
-
Everhart, Joel L., Hollingsworth, Kevin E., Erickson, David W., Merski, N. Ronald, and Prabhu, Ramadas K., "Real-Cavity Heating Experiments Supporting Shuttle Orbiter Return To Flight," NASA JSC EG-SS-07-01, February 2007.
-
(2007)
Real-Cavity Heating Experiments Supporting Shuttle Orbiter Return to Flight
-
-
Everhart, J.L.1
Hollingsworth, K.E.2
Erickson, D.W.3
Merski, N.R.4
Prabhu, R.K.5
-
7
-
-
67650886900
-
The cavity heating tool
-
NASA Space Systems, Houston, TX, Dec. 7
-
Anderson, Brian, Hyatt, Jay, Wang, K.C., Everhart, Joel, Greene, Frank, Pulsonetti, Maria, Wood, Bill, Bourland, Gary, and Cassady, Amy," The Cavity Heating Tool," Boeing Technical Memorandum ATA-AH-TM-2005-079, The Boeing Company, NASA Space Systems, Houston, TX, Dec. 7, 2005.
-
(2005)
Boeing Technical Memorandum ATA-AH-TM-2005-079, the Boeing Company
-
-
Anderson, B.1
Hyatt, J.2
Wang, K.C.3
Everhart, J.4
Greene, F.5
Pulsonetti, M.6
Wood, B.7
Bourland, G.8
Cassady, A.9
-
8
-
-
77958498422
-
Supersonic/hypersonic laminar heating correlations for rectangular and impact-induced open and closed cavities
-
AIAA 2008-1283, Presented at, Reno, NV, January 7-10
-
Everhart, Joel L., "Supersonic/Hypersonic Laminar Heating Correlations for Rectangular and Impact-Induced Open and Closed Cavities," AIAA 2008-1283, Presented at 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 7-10, 2008.
-
(2008)
46th AIAA Aerospace Sciences Meeting and Exhibit
-
-
Everhart, J.L.1
-
11
-
-
0007725154
-
-
NASA TM-2000-210316, Aug
-
Berry, S.A., Difulvio, Michael, and Kowalkowski, Matthew K., "Forced Boundary-Layer Transition on X-43 (Hyper-X) in NASA LaRC 20-Inch Mach 6 Air Tunnel." NASA TM-2000-210316, Aug.2000.
-
(2000)
Forced Boundary-Layer Transition on X-43 (Hyper-X) in NASA LaRC 20-Inch Mach 6 Air Tunnel
-
-
Berry, S.A.1
Difulvio, M.2
Kowalkowski, M.K.3
-
12
-
-
0035518402
-
Hypersonic boundary-layer trip development for hyper-X
-
Berry, S.A., Auslender, A.H., Dilley, A.D., and Calleja, J.J., "Hypersonic Boundary-Layer Trip Development for Hyper-X," Journal of Spacecraft and Rockets, Volume 38, Number 6, pp. 853-864, 2001.
-
(2001)
Journal of Spacecraft and Rockets
, vol.38
, Issue.6
, pp. 853-864
-
-
Berry, S.A.1
Auslender, A.H.2
Dilley, A.D.3
Calleja, J.J.4
-
13
-
-
0002798520
-
-
U.S. Patent 5, 266, 252, November
-
Buck, G.M., and Vasques, P., "An Investment Ceramic Slip-Casting Technique for Net-Form, Precision, Detailed Casting of Ceramic Models," U.S. Patent 5, 266, 252, November 1993.
-
(1993)
An Investment Ceramic Slip-Casting Technique for Net-Form, Precision, Detailed Casting of Ceramic Models
-
-
Buck, G.M.1
Vasques, P.2
-
14
-
-
34250886702
-
-
NASA TM 2006-
-
Buck, G.M., Powers, M.A., Nevins, S.C., Griffith, M.S., Verneris, P.H., and Wainwright, G.A., "Rapid Fabrication of Flat Plate Cavity Phosphor Thermography Test Models for Shuttle Return-to-Flight Aero-Heating," NASA TM 2006-214508.
-
Rapid Fabrication of Flat Plate Cavity Phosphor Thermography Test Models for Shuttle Return-to-Flight Aero-Heating
-
-
Buck, G.M.1
Powers, M.A.2
Nevins, S.C.3
Griffith, M.S.4
Verneris, P.H.5
Wainwright, G.A.6
-
16
-
-
67650902877
-
-
JSC-26816, December
-
Campbell, Charles H., Wang, K. C., An, Michael Y., Tam, Luen T., Bouslog, Stanley A., "Orbiter Boundary-Layer Working Group, Numerical Flow Field Analysis Data," JSC-26816, December, 1994.
-
(1994)
Orbiter Boundary-Layer Working Group, Numerical Flow Field Analysis Data
-
-
Campbell, C.H.1
Wang, K.C.2
An, M.Y.3
Tam, L.T.4
Bouslog, S.A.5
-
17
-
-
0024613058
-
-
NASA TP 2867, February
-
Gnoffo, P.A., Gupta, R.N., and Shinn, J.L., "Conservation Equations and Physical Models for Hypersonic Air Flows in Thermal and Chemical Nonequilibrium," NASA TP 2867, February 1989.
-
(1989)
Conservation Equations and Physical Models for Hypersonic Air Flows in Thermal and Chemical Nonequilibrium
-
-
Gnoffo, P.A.1
Gupta, R.N.2
Shinn, J.L.3
-
18
-
-
85041141206
-
-
NASA TP 2953, February
-
Gnoffo, P.A., An Upwind-Biased, Point-Implicit Relaxation Algorithm for Viscous, Compressible Perfect Gas Flows," NASA TP 2953, February 1990.
-
(1990)
An Upwind-Biased, Point-Implicit Relaxation Algorithm for Viscous, Compressible Perfect Gas Flows
-
-
Gnoffo, P.A.1
-
19
-
-
0024613058
-
-
NASA TP 2867
-
Gnoffo, P. A., Gupta, R. N., and Shinn, J., "Conservation Equations and Physical Models for Hypersonic Air Flows in Thermal and Chemical Nonequilibrium," NASA TP 2867, 1989.
-
(1989)
Conservation Equations and Physical Models for Hypersonic Air Flows in Thermal and Chemical Nonequilibrium
-
-
Gnoffo, P.A.1
Gupta, R.N.2
Shinn, J.3
-
21
-
-
0030109362
-
Influence of sonic-line location on mars pathfinder probe aerothermodynamics
-
Gnoffo, P. A., Weilmuenster, K. J., Braun, R. D., and Cruz, C. I., "Influence of Sonic-Line Location on Mars Pathfinder Probe Aerothermodynamics," Journal of Spacecraft and Rockets, Vol. 33, No. 2, 1996, pp.169-177.
-
(1996)
Journal of Spacecraft and Rockets
, vol.33
, Issue.2
, pp. 169-177
-
-
Gnoffo, P.A.1
Weilmuenster, K.J.2
Braun, R.D.3
Cruz, C.I.4
-
22
-
-
0032625899
-
Prediction and validation of mars pathfinder hypersonic aerodynamic database
-
Gnoffo, P. A., Braun, R. D., Weilmuenster, K. J., Mitcheltree, R. A., Engelund, W. C., and Powell, R. W., "Prediction and Validation of Mars Pathfinder Hypersonic Aerodynamic Database," Journal of Spacecraft and Rockets, Vol. 36, No. 3, 1999, pp. 367-373.
-
(1999)
Journal of Spacecraft and Rockets
, vol.36
, Issue.3
, pp. 367-373
-
-
Gnoffo, P.A.1
Braun, R.D.2
Weilmuenster, K.J.3
Mitcheltree, R.A.4
Engelund, W.C.5
Powell, R.W.6
-
23
-
-
0026715316
-
Application of the LAURA code for slender-vehicle aerothermodynamics
-
Thompson, R. A., Gnoffo, P. A., "Application of the LAURA Code for Slender-Vehicle Aerothermodynamics," Journal of Spacecraft and Rockets, Vol. 29, No. 1, 1992, pp. 16-23.
-
(1992)
Journal of Spacecraft and Rockets
, vol.29
, Issue.1
, pp. 16-23
-
-
Thompson, R.A.1
Gnoffo, P.A.2
-
24
-
-
2942757053
-
Approximate Riemann solvers, parameter vectors and difference schemes
-
Roe, P. L., "Approximate Riemann Solvers, Parameter Vectors and Difference Schemes," Journal of Computational Physics, Vol. 43, No. 2, 1981, pp. 357-372.
-
(1981)
Journal of Computational Physics
, vol.43
, Issue.2
, pp. 357-372
-
-
Roe, P.L.1
-
25
-
-
40749159424
-
High resolution schemes for hyperbolic conservation laws
-
Harten, A., "High Resolution Schemes for Hyperbolic Conservation Laws," Journal of Computational Physics, Vol. 49, No. 3, 1983, pp. 357-393.
-
(1983)
Journal of Computational Physics
, vol.49
, Issue.3
, pp. 357-393
-
-
Harten, A.1
-
27
-
-
0014893119
-
Behavior of turbulent flow near a porous wall with pressure gradient
-
December
-
Cebeci, T. "Behavior of Turbulent Flow near a Porous Wall with Pressure Gradient," AIAA Journal, Vol. 8, No. 12, December 1970, pp. 2152-2156.
-
(1970)
AIAA Journal
, vol.8
, Issue.12
, pp. 2152-2156
-
-
Cebeci, T.1
-
28
-
-
0004254511
-
-
Prentice-Hall, Inc. Englewood Cliffs, New Jersey
-
Morrison, Donald F., "Applied Linear Statistical Methods," Prentice-Hall, Inc., Englewood Cliffs, New Jersey, 1983.
-
(1983)
Applied Linear Statistical Methods
-
-
Morrison, D.F.1
-
29
-
-
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
-
30
-
-
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., 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, pp. 513-527, July 1961.
-
(1961)
Journal of Aerospace Sciences
, vol.28
, Issue.7
, pp. 513-527
-
-
Charwat, A.F.1
Dewey, C.F.2
Roos, J.N.3
Hitz, J.A.4
-
31
-
-
34250894211
-
Recompression step heat transfer coefficients for supersonic open cavity flow
-
Emery, A.F.: "Recompression Step Heat Transfer Coefficients for Supersonic Open Cavity Flow," Journal of Heat Transfer, 1969, pp. 168-170.
-
(1969)
Journal of Heat Transfer
, pp. 168-170
-
-
Emery, A.F.1
-
32
-
-
85007072207
-
Experiment and computation in hypersonic cavity flows
-
AIAA Paper 89-1842, Presented at, Buffalo, NY, June 12-14
-
Netterfield, M. and Hillier, R.: "Experiment and Computation in Hypersonic Cavity Flows," AIAA Paper 89-1842, Presented at 20th Fluid Dynamics, Plasma Dynamics and Lasers Conference, Buffalo, NY, June 12-14, 1989.
-
(1989)
20th Fluid Dynamics, Plasma Dynamics and Lasers Conference
-
-
Netterfield, M.1
Hillier, R.2
-
34
-
-
85007683104
-
Experimental investigation of separated flows over a cavity at hypersonic speed
-
AIAA No. 68-672, June
-
Hahn, Mansop: "Experimental Investigation of Separated Flows over a Cavity at Hypersonic Speed," AIAA No. 68-672, AIAA Journal, Vol. 7, No. 6, June 1969, pp. 1092-1098.
-
(1969)
AIAA Journal
, vol.7
, Issue.6
, pp. 1092-1098
-
-
Hahn, M.1
-
35
-
-
33947226905
-
Heat transfer to steps and cavities in hypersonic turbulent flow
-
AIAA Paper No. 68-673, Presented at, Los Angeles, Calif
-
Nestler, D.E., Saydah, A.R., and Auxer, W.L.: "Heat Transfer to Steps and Cavities in Hypersonic Turbulent Flow," AIAA Paper No. 68-673, Presented at Fluid and Plasma Dynamics Conference, Los Angeles, Calif., 1968.
-
(1968)
Fluid and Plasma Dynamics Conference
-
-
Nestler, D.E.1
Saydah, A.R.2
Auxer, W.L.3
-
36
-
-
0004108629
-
-
First Edition, McGraw-Hill Book Company
-
White, F. M.: "Viscous Fluid Flow", First Edition, McGraw-Hill Book Company, 1974.
-
(1974)
Viscous Fluid Flow
-
-
White, F.M.1
|