-
1
-
-
84982318478
-
-
AIAA Paper 98-0868, Jan
-
Prabhu, D. K., Loomis, M. P., Venkatapathy, E., Polsky, S., Papadopoulos, P., Davies, C. B., and Henline, W. D., "X-33 Aerothermal Environment Simulations and Aerothermodynamic Design, " AIAA Paper 98-0868, Jan. 1998.
-
(1998)
X-33 Aerothermal Environment Simulations and Aerothermodynamic Design
-
-
Prabhu, D.K.1
Loomis, M.P.2
Venkatapathy, E.3
Polsky, S.4
Papadopoulos, P.5
Davies, C.B.6
Henline, W.D.7
-
2
-
-
2942751073
-
-
AeroSoft, Inc., 1872 Pratt Drive, Blacksburg, VA 24060-6363
-
AeroSoft, Inc., 1872 Pratt Drive, Blacksburg, VA 24060-6363, GASPex Version 3 User's Manual, 1996.
-
(1996)
GASPex Version 3 User's Manual
-
-
-
3
-
-
33846072059
-
-
AIAA Paper 98-0870. Jan
-
Bowles. J. V., Henline, W. D., Huynh, L. C., Davies, C. B., Roberts. C D., and Yang, L. H., "Development of an Aerother-modynamic Environments Database for the Integrated Design of the Prototype Flight Tests Vehicle. " AIAA Paper 98-0870. Jan. 1998.
-
(1998)
Development of an Aerother-modynamic Environments Database for the Integrated Design of the Prototype Flight Tests Vehicle
-
-
Bowles, J.V.1
Henline, W.D.2
Huynh, L.C.3
Davies, C.B.4
Roberts, C.D.5
Yang, L.H.6
-
4
-
-
84894533443
-
-
AIAA Paper 2000-2687, June
-
Kontinos, D., Wright, M., Prabhu, D., and Venkatapathy, E., "X-33 Aerothermal Environment Predictions: Review and Special Topics, " AIAA Paper 2000-2687, June 2000
-
(2000)
X-33 Aerothermal Environment Predictions: Review and Special Topics
-
-
Kontinos, D.1
Wright, M.2
Prabhu, D.3
Venkatapathy, E.4
-
5
-
-
0345160664
-
-
AIAA Paper 95-2079, June
-
Henline, W. D., Palmer, G. E., Milos, F. S., Olynick, D, R., and Chen, Y.-K., "Aerothermodynamic Heating Analysis and Heatshield Design of an SSTO Rocket Vehicle for Access-to-Space. " AIAA Paper 95-2079, June 1995.
-
(1995)
Aerothermodynamic Heating Analysis and Heatshield Design of an SSTO Rocket Vehicle for Access-to-Space
-
-
Henline, W.D.1
Palmer, G.E.2
Milos, F.S.3
Olynick, D.R.4
Chen, Y.-K.5
-
6
-
-
0030243259
-
Guide to Credible Computer Simulations of Fluid Flows
-
Mehta, U. B., "Guide to Credible Computer Simulations of Fluid Flows. " Journal of Propulsion and Power, Vol. 12, No. 5, 1996. pp. 940-948.
-
(1996)
Journal of Propulsion and Power
, vol.12
, Issue.5
, pp. 940-948
-
-
Mehta, U.B.1
-
8
-
-
0031100517
-
Trajectory-Based Validation of the Shuttle Heating Environment
-
Olynick, D. R. and Tam, T. "Trajectory-Based Validation of the Shuttle Heating Environment, " Journal of Spacecraft and Rockets. Vol. 34, No. 2, 1997, pp. 172-181.
-
(1997)
Journal of Spacecraft and Rockets.
, vol.34
, Issue.2
, pp. 172-181
-
-
Olynick, D.R.1
Tam, T.2
-
9
-
-
0007823326
-
-
AIAA Paper 97-2478, June
-
Loomis, M. P. Venkatapathy, E., Papadopoulos, P., Davies. C. B., Berry, S. A., Horvath, T., and Campbell, C., "Aeroheating and Aerodynamic CFD Validation and Prediction for the X-38 Program, " AIAA Paper 97-2478, June 1997.
-
(1997)
Aeroheating and Aerodynamic CFD Validation and Prediction for the X-38 Program
-
-
Loomis, M.P.1
Venkatapathy, E.2
Papadopoulos, P.3
Davies, C.B.4
Berry, S.A.5
Horvath, T.6
Campbell, C.7
-
10
-
-
0033099530
-
A Heating Analysis of the Nosecap and Leading Edges of the X-34 Vehicle
-
Palmer, G. E. and Polsky, S., "A Heating Analysis of the Nosecap and Leading Edges of the X-34 Vehicle. " Journal of Spacecraft and Rockets, Vol. 36, No. 2, 1999, pp. 199-205.
-
(1999)
Journal of Spacecraft and Rockets
, vol.36
, Issue.2
, pp. 199-205
-
-
Palmer, G.E.1
Polsky, S.2
-
11
-
-
2942723480
-
-
AIAA Paper 99-3560, June
-
Berry. S. A., Horvath, T. J., Hollis, B. R., Thompson, R. A., and Hamilton, H. H., II, "X-33 Hypersonic Boundary Layer Transition. " AIAA Paper 99-3560, June 1999.
-
(1999)
X-33 Hypersonic Boundary Layer Transition
-
-
Berry, S.A.1
Horvath, T.J.2
Hollis, B.R.3
Thompson, R.A.4
Hamilton II, H.H.5
-
12
-
-
0004256918
-
Hypersonic Aerothermodynamics
-
AIAA. Washington, DC
-
Bertin, J. J., Hypersonic Aerothermodynamics. AIAA Education Series, AIAA. Washington, DC, 1994.
-
(1994)
AIAA Education Series
-
-
Bertin, J.J.1
-
13
-
-
0003957554
-
-
Report SC-RR-70-754, Sandia Laboratories, Albuquerque, NM. Dec
-
Blottner, F. G., Johnson, M., and Ellis, M., "Chemically Reacting Viscous Flow Program for Multi-Component Gas Mixtures, " Report SC-RR-70-754, Sandia Laboratories, Albuquerque, NM. Dec. 1971
-
(1971)
Chemically Reacting Viscous Flow Program for Multi-Component Gas Mixtures
-
-
Blottner, F.G.1
Johnson, M.2
Ellis, M.3
-
14
-
-
0000227509
-
On the Heat Conductivity, the Specific Heat, and the Internal Friction of Gases
-
Eucken. A., "On the Heat Conductivity, the Specific Heat, and the Internal Friction of Gases, " Physikalische Zeitschnft, Vol 14, 1913, pp. 324-332
-
(1913)
Physikalische Zeitschnft
, vol.14
, pp. 324-332
-
-
Eucken, A.1
-
15
-
-
34347366615
-
A Viscosity Equation for Gas Mixtures
-
Wilke, C. R., "A Viscosity Equation for Gas Mixtures, " Journal of Chemical Physics, Vol. 18, 1950, pp. 517-519.
-
(1950)
Journal of Chemical Physics
, vol.18
, pp. 517-519
-
-
Wilke, C.R.1
-
16
-
-
0027626879
-
Review of Chemical-Kinetic Problems of Future NASA Missions, I: Earth Entries
-
Park, C., "Review of Chemical-Kinetic Problems of Future NASA Missions, I: Earth Entries, " Journal of Thermophysics and Heat Transfer, Vol. 7, No. 3. 1993, pp. 385-398.
-
(1993)
Journal of Thermophysics and Heat Transfer
, vol.7
, Issue.3
, pp. 385-398
-
-
Park, C.1
-
18
-
-
84982319119
-
-
AIAA Paper 98-2844, June
-
Prabhu, D. K., Venkatapathy, E., Kontinos, D. A., and Papadopoulos, P., "X-33 Catalytic Heating, " AIAA Paper 98-2844, June 1998.
-
(1998)
X-33 Catalytic Heating
-
-
Prabhu, D.K.1
Venkatapathy, E.2
Kontinos, D.A.3
Papadopoulos, P.4
-
19
-
-
84894594511
-
Evaluation of CFD Requirements and Accuracy for Prediction of Reentry Heating Environments
-
Wilson, G. J., Lawrence, S. L., Venkatapathy, E., Polsky, S., Papadopoulos. P., Sussman, M. A., and Henline, W. D., "Evaluation of CFD Requirements and Accuracy for Prediction of Reentry Heating Environments. " Unpublished Internal Report (restricted due to Competition Sensitive Technology).
-
Unpublished Internal Report (restricted due to Competition Sensitive Technology)
-
-
Wilson, G.J.1
Lawrence, S.L.2
Venkatapathy, E.3
Polsky, S.4
Papadopoulos, P.5
Sussman, M.A.6
Henline, W.D.7
-
21
-
-
0001642656
-
Flux-Split Algorithms for Flows with Non-Equilibrium Chemistry and Vibrational Relaxation
-
Grossman, B. and Cinnella, P., "Flux-Split Algorithms for Flows with Non-Equilibrium Chemistry and Vibrational Relaxation, " Journal of Computational Physics, Vol. 88, 1990. pp. 131-168.
-
(1990)
Journal of Computational Physics
, vol.88
, pp. 131-168
-
-
Grossman, B.1
Cinnella, P.2
-
22
-
-
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
-
23
-
-
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
-
25
-
-
2442433925
-
Towards the Ultimate Conservative Difference Scheme V". A Second-Order Sequel to Godunov's Method
-
van Leer, B., "Towards the Ultimate Conservative Difference Scheme V". A Second-Order Sequel to Godunov's Method, " Journal of Computational Physics. Vol. 32. 1979, pp 101-136.
-
(1979)
Journal of Computational Physics.
, vol.32
, pp. 101-136
-
-
van Leer, B.1
-
26
-
-
0004201353
-
-
Academic Press, New York, NY
-
Cebeci, T. and Smith, A. M. O., Analysis of Turbulent Boundary Layers, Academic Press, New York, NY, 1974.
-
(1974)
Analysis of Turbulent Boundary Layers
-
-
Cebeci, T.1
Smith, A.M.O.2
-
27
-
-
0001519438
-
On Turbulent Flow Near a Wall
-
Nov
-
van Driest, E. R., "On Turbulent Flow Near a Wall, " Journal of the Aeronautical Sciences, Vol. 23, No. 11, Nov. 1956, pp 1007-1011,1036.
-
(1956)
Journal of the Aeronautical Sciences
, vol.23
, Issue.11
-
-
van Driest, E.R.1
-
29
-
-
0025405279
-
Hypersonic Viscous Shock-Layer Solutions over Long Slender Bodies-Part I: High Reynolds Number Flows
-
Gupta, R. N., Lee, K. P., Zoby, E. V., Moss. J. N., and Thompson, R. A., "Hypersonic Viscous Shock-Layer Solutions over Long Slender Bodies-Part I: High Reynolds Number Flows, " Journal of Spacecraft and Rockets, Vol. 27, No. 2, 1990, pp. 175-184.
-
(1990)
Journal of Spacecraft and Rockets
, vol.27
, Issue.2
, pp. 175-184
-
-
Gupta, R.N.1
Lee, K.P.2
Zoby, E.V.3
Moss, J.N.4
Thompson, R.A.5
-
30
-
-
0002046089
-
The Problem of Aerodynamic Heating
-
Oct
-
van Driest, E. R., "The Problem of Aerodynamic Heating, " Aeronautical Eng. Rev., Vol. 15, No. 10, Oct. 1956, pp. 26-41.
-
(1956)
Aeronautical Eng. Rev.
, vol.15
, Issue.10
, pp. 26-41
-
-
van Driest, E.R.1
-
32
-
-
0028423185
-
Approximate Method for Calculating Heating Rates on Three-Dimensional Vehicles
-
Hamilton. H. H., II, A. Greene, F., and DeJarnette, F. R., "Approximate Method for Calculating Heating Rates on Three-Dimensional Vehicles, " Journal of Spacecraft and Rockets, Vol. 31, No. 3, 1994, pp. 345-354.
-
(1994)
Journal of Spacecraft and Rockets
, vol.31
, Issue.3
, pp. 345-354
-
-
Hamilton II, H.H.1
Greene, A.F.2
DeJarnette, F.R.3
-
33
-
-
85088767552
-
-
AIAA Paper 98-0867, Jan
-
Thompson, R. A., Hamilton, H. H., II, Berry, S. A., Horvath, T. J., and Nowak, R. J., "Hypersonic Boundary Layer Transition for X-33 Phase II Vehicle, " AIAA Paper 98-0867, Jan. 1998.
-
(1998)
Hypersonic Boundary Layer Transition for X-33 Phase II Vehicle
-
-
Thompson, R.A.1
Hamilton II, H.H.2
Berry, S.A.3
Horvath, T.J.4
Nowak, R.J.5
-
34
-
-
84877369015
-
-
Pointwise, inc., PO Box 210698, Bedford, TX 76095-7698
-
Pointwise, inc., PO Box 210698, Bedford, TX 76095-7698, Gridgen User Manual version 12, 1997.
-
(1997)
Gridgen User Manual version 12
-
-
-
35
-
-
0003866745
-
-
NASA TM 108791
-
Chan, W. M., Chiu, I. T., and Buning, P. G., "User's Manual for the HYPGEN Hyperbolic Grid Generator and the HGUI Graphical User Interface, " NASA TM 108791, 1993.
-
(1993)
User's Manual for the HYPGEN Hyperbolic Grid Generator and the HGUI Graphical User Interface
-
-
Chan, W.M.1
Chiu, I.T.2
Buning, P.G.3
-
36
-
-
84894548313
-
-
Altair Computing, Inc., 1757 Maplelawn Drive, Troy, MI 48084
-
Altair Computing, Inc., 1757 Maplelawn Drive, Troy, MI 48084, Hyper Mesh® 2.1 User's Manual, 1997.
-
(1997)
Hyper Mesh® 2.1 User's Manual
-
-
-
37
-
-
0004273471
-
-
Program Development Corp., 300 Hamilton Avenue, Suite 409, White Plains, NY 10601
-
Program Development Corp., 300 Hamilton Avenue, Suite 409, White Plains, NY 10601, GridPro™/az3000-User's Guide and Reference Manual, 1996.
-
(1996)
GridPro™/az3000-User's Guide and Reference Manual
-
-
-
38
-
-
0038511691
-
-
NASA TM 1999-208792, Aug
-
Davies, C. B. and Venkatapathy, E., "The Self-Adaptive Grid codE, SAGE, Version 3, " NASA TM 1999-208792, Aug. 1999.
-
(1999)
The Self-Adaptive Grid codE, SAGE, Version 3
-
-
Davies, C.B.1
Venkatapathy, E.2
-
39
-
-
0033451188
-
Current Grid-Generation Strategies and Future Requirements in Hypersonic Vehicle Design, Analysis and Testing
-
Papadopoulos, P., Venkatapathy, E., Prabhu, D., Loomis. M., and Olynick, D., "Current Grid-Generation Strategies and Future Requirements in Hypersonic Vehicle Design, Analysis and Testing, " Applied Mathematical Modelling, Vol. 23, 1999, pp. 705-735.
-
(1999)
Applied Mathematical Modelling
, vol.23
, pp. 705-735
-
-
Papadopoulos, P.1
Venkatapathy, E.2
Prabhu, D.3
Loomis, M.4
Olynick, D.5
-
40
-
-
0002887728
-
Theory of Stagnation Point Heat Transfer in Dissociated Air
-
Fay, J. A. and Riddell, F. R., "Theory of Stagnation Point Heat Transfer in Dissociated Air, " Journal of the Aeronautical Sciences, Vol. 25, No. 2, 1958, pp. 73-85.
-
(1958)
Journal of the Aeronautical Sciences
, vol.25
, Issue.2
, pp. 73-85
-
-
Fay, J.A.1
Riddell, F.R.2
-
41
-
-
84894560442
-
-
AIAA Paper 99-3558, June
-
Horvath, T. J., Berry, S. A., Hollis, B. R., Liechty, D. S., Hamilton, H. H., II, and Merski, N. R., "X-33 Experimental Aeroheating at Mach 6 Using Phosphor Thermography, " AIAA Paper 99-3558, June 1999.
-
(1999)
X-33 Experimental Aeroheating at Mach 6 Using Phosphor Thermography
-
-
Horvath, T.J.1
Berry, S.A.2
Hollis, B.R.3
Liechty, D.S.4
Hamilton II, H.H.5
Merski, N.R.6
-
42
-
-
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, 1999, pp. 160-170.
-
(1999)
Journal of Spacecraft and Rockets
, vol.36
, Issue.2
, pp. 160-170
-
-
Merski, N.R.1
-
44
-
-
43749122910
-
-
AIAA Paper 99-3559, June
-
Hollis, B. R., Horvath, T. J., Berry, S. A., Hamilton, H. H., II, and Halter, S. J., "X-33 Computational Aeroheating Predictions and Comparisons with Experimental Data, " AIAA Paper 99-3559, June 1999.
-
(1999)
X-33 Computational Aeroheating Predictions and Comparisons with Experimental Data
-
-
Hollis, B.R.1
Horvath, T.J.2
Berry, S.A.3
Hamilton II, H.H.4
Halter, S.J.5
-
46
-
-
84983119810
-
-
AIAA Paper 98-0881, Jan
-
Berry, S. A., Horvath, T. J., DiFulvio, M., Glass, C. E., and Merski, N. R., "X-34 Experimental Aeroheating at Mach 6 and 10, " AIAA Paper 98-0881, Jan. 1998.
-
(1998)
X-34 Experimental Aeroheating at Mach 6 and 10
-
-
Berry, S.A.1
Horvath, T.J.2
DiFulvio, M.3
Glass, C.E.4
Merski, N.R.5
-
47
-
-
0011717911
-
-
AIAA Paper 87-1112, June
-
Lawrence. S. L., Chaussee, D. S., and Tannehill, J. C., "Application of an Upwind Algorithm to the Three-Dimensional Parabolized Navier-Stokes Equations, " AIAA Paper 87-1112, June 1987
-
(1987)
Application of an Upwind Algorithm to the Three-Dimensional Parabolized Navier-Stokes Equations
-
-
Lawrence, S.L.1
Chaussee, D.S.2
Tannehill, J.C.3
-
48
-
-
0026626816
-
Flow over an All-Body Hypersonic Aircraft: Experiment and Computation
-
Lockman, W. K., Lawrence, S. L., and Cleary, J. W., "Flow over an All-Body Hypersonic Aircraft: Experiment and Computation, " Journal of Spacecraft and Rockets, Vol. 29, No. 1, 1992, pp. 7-15.
-
(1992)
Journal of Spacecraft and Rockets
, vol.29
, Issue.1
, pp. 7-15
-
-
Lockman, W.K.1
Lawrence, S.L.2
Cleary, J.W.3
-
50
-
-
0003432880
-
-
Anon., NACA Report 1135, NASA Ames Research Center
-
Anon., "Equations, Tables, and Charts for Compressible Flow, " NACA Report 1135, NASA Ames Research Center, 1953.
-
(1953)
Equations, Tables, and Charts for Compressible Flow
-
-
-
51
-
-
0032734289
-
Computational Aerothermodynamic Design Issues for Hypersonic Vehicles
-
Gnoffo, P. A., Weilmuenster, K. J., Hamilton, H. H., II, Olynick. D. R, and Venkatapathy, E., "Computational Aerothermodynamic Design Issues for Hypersonic Vehicles, " Journal of Spacecraft and Rockets, Vol. 36. No. 1. 1999, pp. 21-43
-
(1999)
Journal of Spacecraft and Rockets
, vol.36
, Issue.1
, pp. 21-43
-
-
Gnoffo, P.A.1
Weilmuenster, K.J.2
Hamilton II, H.H.3
Olynick, D.R.4
Venkatapathy, E.5
-
52
-
-
84983140092
-
-
AIAA Paper 98-0865, Jan
-
Palmer, G., Kontinos, D., and Sherman, B., "Surface Heating Effects of X-33 Vehicle TPS Panel Bowing, Steps, and Gaps, " AIAA Paper 98-0865, Jan. 1998.
-
(1998)
Surface Heating Effects of X-33 Vehicle TPS Panel Bowing, Steps, and Gaps
-
-
Palmer, G.1
Kontinos, D.2
Sherman, B.3
-
53
-
-
0033358327
-
Numerical Simulation of Metallic Thermal Protection System Panel Bowing
-
Kontinos, D. A., and Palmer, G., "Numerical Simulation of Metallic Thermal Protection System Panel Bowing, " Journal of Spacecraft and Rockets, Vol. 36, No. 6, 1999, pp. 842-849.
-
(1999)
Journal of Spacecraft and Rockets
, vol.36
, Issue.6
, pp. 842-849
-
-
Kontinos, D.A.1
Palmer, G.2
-
55
-
-
84964054284
-
-
AIAA Paper 97-2475, June
-
Campbell, C., Caram, J., Berry, S., Horvath, T., Merski, N., Loomis. M., and Venkatapathy, E., "Overview of X-38 Hypersonic Aerothermodynamic Wind Tunnel Data and Comparison with Numerical Results, " AIAA Paper 97-2475, June 1997
-
(1997)
Overview of X-38 Hypersonic Aerothermodynamic Wind Tunnel Data and Comparison with Numerical Results
-
-
Campbell, C.1
Caram, J.2
Berry, S.3
Horvath, T.4
Merski, N.5
Loomis, M.6
Venkatapathy, E.7
-
56
-
-
0028338141
-
Characteristics of the Shuttle Orbiter Leeside Flow During a Reentry Condition
-
Kleb, W. L. and Weilmuenster, K. J., "Characteristics of the Shuttle Orbiter Leeside Flow During a Reentry Condition, " Journal of Spacecraft and Rockets, Vol. 31, No. 1, 1994, pp. 8-16.
-
(1994)
Journal of Spacecraft and Rockets
, vol.31
, Issue.1
, pp. 8-16
-
-
Kleb, W.L.1
Weilmuenster, K.J.2
-
57
-
-
0003592561
-
-
NASA RP 1311, Oct
-
Gordon, S. G. and McBride, B. J., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications, I: Analysis, " NASA RP 1311, Oct. 1994.
-
(1994)
Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications, I: Analysis
-
-
Gordon, S.G.1
McBride, B.J.2
-
58
-
-
0004079116
-
-
McGraw-Hill, New York, NY
-
Anderson, Jr., J. D., Hypersonic and High Temperature Gas Dynamics, McGraw-Hill, New York, NY, 1989.
-
(1989)
Hypersonic and High Temperature Gas Dynamics
-
-
Anderson Jr., J.D.1
|