-
2
-
-
0345703777
-
-
AIAA Paper 95-2081, June
-
Chen, Y.-K., Henline, W. D., Olynick, D. R., and Palmer, G. E., "Three-Dimensional Hypersonic Flowfields and Heating Analysis over the DC-3 Vehicle," AIAA Paper 95-2081, June 1995.
-
(1995)
Three-Dimensional Hypersonic Flowfields and Heating Analysis over the DC-3 Vehicle
-
-
Chen, Y.-K.1
Henline, W.D.2
Olynick, D.R.3
Palmer, G.E.4
-
3
-
-
0345160664
-
-
AIAA Paper 95-2079, June
-
Henline, W. D., Palmer, G. E., 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
Olynick, D.R.3
Chen, Y.-K.4
-
4
-
-
3943094667
-
-
AIAA Paper 95-2080, June
-
Palmer, G. E., Henline, W. D., Olynick, D. R., and Chen, Y.-K., "Heating Analysis of a Lifting Body Single-Stage-to-Orbit Vehicle," AIAA Paper 95-2080, June 1995.
-
(1995)
Heating Analysis of a Lifting Body Single-Stage-to-Orbit Vehicle
-
-
Palmer, G.E.1
Henline, W.D.2
Olynick, D.R.3
Chen, Y.-K.4
-
5
-
-
0029277402
-
Trajectory Based Heating and Ablation Calculations for Mars/Pathfinder Aeroshell
-
Chen, Y.-K., Henline, W. D., and Tauber, M. E., "Trajectory Based Heating and Ablation Calculations for Mars/Pathfinder Aeroshell," Journal of Spacecraft and Rockets, Vol. 32, No. 2, 1995, pp. 225-230.
-
(1995)
Journal of Spacecraft and Rockets
, vol.32
, Issue.2
, pp. 225-230
-
-
Chen, Y.-K.1
Henline, W.D.2
Tauber, M.E.3
-
6
-
-
33644777991
-
-
Wiley, New York
-
Hirsch, C., Numerical Computation of Internal and External Flows, Vol. 2: Computation Methods for Inviscid and Viscous Flows, 1st ed., Wiley, New York, 1990, pp. 493-583.
-
(1990)
Numerical Computation of Internal and External Flows, Vol. 2: Computation Methods for Inviscid and Viscous Flows, 1st Ed.
, vol.2
, pp. 493-583
-
-
Hirsch, C.1
-
8
-
-
0028423169
-
Multiblock Analysis for Shuttle Orbiter Re-entry Heating from Mach 24 to Mach 12
-
Gnoffo, P. A., Weilmuenster, K. J., and Alter, S. J., "Multiblock Analysis for Shuttle Orbiter Re-entry Heating from Mach 24 to Mach 12," Journal of Spacecraft and Rockets, Vol. 31, No. 3, 1994, pp. 385-394.
-
(1994)
Journal of Spacecraft and Rockets
, vol.31
, Issue.3
, pp. 385-394
-
-
Gnoffo, P.A.1
Weilmuenster, K.J.2
Alter, S.J.3
-
9
-
-
0343949455
-
-
AeroSoft, Inc., Blacksburg, VA
-
McGrory, D. M., Slack, D. C., Applebaum, M. P., and Walters, R. W., "GASP Version 2.2: User's Manual," AeroSoft, Inc., Blacksburg, VA, 1993.
-
(1993)
GASP Version 2.2: User's Manual
-
-
McGrory, D.M.1
Slack, D.C.2
Applebaum, M.P.3
Walters, R.W.4
-
10
-
-
0024613058
-
-
NASA TP-2867, Feb.
-
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, Feb. 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
-
12
-
-
0029386232
-
Comparisons of Coupled Radiative Flow Solutions with Project Fire II Flight Data
-
Olynick, D. R., Henline, W. D., Chamber, L. H., and Candler, G. V., "Comparisons of Coupled Radiative Flow Solutions with Project Fire II Flight Data," Journal of Thermophysics and Heat Transfer, Vol. 9, No. 4, 1995, pp. 586-594.
-
(1995)
Journal of Thermophysics and Heat Transfer
, vol.9
, Issue.4
, pp. 586-594
-
-
Olynick, D.R.1
Henline, W.D.2
Chamber, L.H.3
Candler, G.V.4
-
13
-
-
0003575163
-
-
Ph.D. Thesis, Dept. of Aeronautics and Astronautics, Stanford Univ., Stanford, CA, June
-
Candler, G. V., "The Computation of Weakly Ionized Hypersonic Flows in Chemical Nonequilibrium," Ph.D. Thesis, Dept. of Aeronautics and Astronautics, Stanford Univ., Stanford, CA, June 1988.
-
(1988)
The Computation of Weakly Ionized Hypersonic Flows in Chemical Nonequilibrium
-
-
Candler, G.V.1
-
14
-
-
0003894360
-
-
NASA RP-1232, Aug.
-
Gupta, R. N., Yos, J. M., Thompson, R. A., and Lee, K., "A Review of Reaction Rates and Thermodynamic and Transport Properties for an 11-Species Air Model for Chemical and Thermal Nonequilibrium Calculations to 30,000 K," NASA RP-1232, Aug. 1990.
-
(1990)
A Review of Reaction Rates and Thermodynamic and Transport Properties for An 11-Species Air Model for Chemical and Thermal Nonequilibrium Calculations to 30,000 K
-
-
Gupta, R.N.1
Yos, J.M.2
Thompson, R.A.3
Lee, K.4
-
15
-
-
4243168242
-
-
private communication, Computational Chemistry Branch, NASA Ames Research Center, Moffett Field, CA, June
-
James Stallcop, private communication, Computational Chemistry Branch, NASA Ames Research Center, Moffett Field, CA, June 1993.
-
(1993)
-
-
Stallcop, J.1
-
16
-
-
0001842706
-
Basic Governing Equations for the Flight Regimes of Aeroassisted Orbital Transfer Vehicles
-
edited by H. F. Nelson, Progress in Astronautics and Aeronautics, AIAA, New York
-
Lee, J.-H., "Basic Governing Equations for the Flight Regimes of Aeroassisted Orbital Transfer Vehicles," Thermal Design of Aeroassited Orbital Transfer Vehicles, edited by H. F. Nelson, Vol. 96, Progress in Astronautics and Aeronautics, AIAA, New York, 1985, pp. 3-53.
-
(1985)
Thermal Design of Aeroassited Orbital Transfer Vehicles
, vol.96
, pp. 3-53
-
-
Lee, J.-H.1
-
17
-
-
0042938945
-
-
NASA CR-1063, June
-
Bartlett, E. P., Kendal, R. M., and Rindal, R. A., "An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator: Part IV - A Unified Approximation for Mixture Transport Properties for Multicomponent Boundary-Layer Applications," NASA CR-1063, June 1968.
-
(1968)
An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator: Part IV - A Unified Approximation for Mixture Transport Properties for Multicomponent Boundary-Layer Applications
-
-
Bartlett, E.P.1
Kendal, R.M.2
Rindal, R.A.3
-
18
-
-
85006925387
-
-
AIAA Paper 94-2412, June
-
Desmeuzes, C., Duffa, G., and Dubroca, B., "Different Levels of Modelization for Diffusion Phenomena in Neutral and Ionized Mixtures," AIAA Paper 94-2412, June 1994.
-
(1994)
Different Levels of Modelization for Diffusion Phenomena in Neutral and Ionized Mixtures
-
-
Desmeuzes, C.1
Duffa, G.2
Dubroca, B.3
-
19
-
-
34347366615
-
A Viscosity Equation for Gas Mixtures
-
Wilke, C. R., "A Viscosity Equation for Gas Mixtures," Journal of Chemical Physics, Vol. 18, No. 4, 1950, p. 517.
-
(1950)
Journal of Chemical Physics
, vol.18
, Issue.4
, pp. 517
-
-
Wilke, C.R.1
-
20
-
-
0003957554
-
-
Sandia Labs., Rept. SC-RR-70-754, Albuquerque, NM, Dec.
-
Blottner, F. G., Johnson, M., and Ellis, M., "Chemically Reacting Viscous Flow Program for Multi-Component Gas Mixtures," Sandia Labs., Rept. SC-RR-70-754, 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
-
21
-
-
0028132507
-
Review of Numerical Procedures for Computational Surface Thermochemistry
-
Milos, F. S., and Rasky, D. J., "Review of Numerical Procedures for Computational Surface Thermochemistry," Journal of Thermophysics and Heat Transfer, Vol. 8, No. 1, 1994, pp. 24-34.
-
(1994)
Journal of Thermophysics and Heat Transfer
, vol.8
, Issue.1
, pp. 24-34
-
-
Milos, F.S.1
Rasky, D.J.2
-
22
-
-
0343563093
-
Flight Experiment Demonstrating the Effect of Surface Catalysis on the Heating Distribution over the Space Shuttle Heat Shield
-
edited by David A. Throckmorton, NASA CP-3248, April
-
Stewart, D. A., Rakich, J. V., and Chen, Y.-K., "Flight Experiment Demonstrating the Effect of Surface Catalysis on the Heating Distribution over the Space Shuttle Heat Shield," Orbiter Experiments (OEX) Aerothermodynamics Symposium, edited by David A. Throckmorton, NASA CP-3248, Pt. 2, April 1993, pp. 677-702.
-
(1993)
Orbiter Experiments (OEX) Aerothermodynamics Symposium
, Issue.2 PART
, pp. 677-702
-
-
Stewart, D.A.1
Rakich, J.V.2
Chen, Y.-K.3
-
23
-
-
4243078849
-
-
Ph.D Thesis, Dept. of Mechanical and Aerospace Engineering, North Carolina State Univ., Raleigh, NC, Dec.
-
Olynick, D. R., "A New LU-SGS Flow Solver for Calculating Reentry Flows," Ph.D Thesis, Dept. of Mechanical and Aerospace Engineering, North Carolina State Univ., Raleigh, NC, Dec. 1992.
-
(1992)
A New LU-SGS Flow Solver for Calculating Reentry Flows
-
-
Olynick, D.R.1
-
24
-
-
0028410835
-
Comparisons between DSMC and the Navier-Stokes Equations for Reentry Flows
-
Olynick, D. R., Taylor, J. C., and Hassan, H. A., "Comparisons Between DSMC and the Navier-Stokes Equations for Reentry Flows," Journal of Thermophysics and Heat Transfer, Vol. 8, No. 2, 1994, pp. 251-258.
-
(1994)
Journal of Thermophysics and Heat Transfer
, vol.8
, Issue.2
, pp. 251-258
-
-
Olynick, D.R.1
Taylor, J.C.2
Hassan, H.A.3
-
25
-
-
0002887728
-
Theory of Stagnation-Point Heat Transfer in Dissociated Air
-
Fay, J. A., and Ridell, F. R., "Theory of Stagnation-Point Heat Transfer in Dissociated Air," Journal of Aerospace Sciences, Vol. 25, No. 2, 1958, pp. 54-67.
-
(1958)
Journal of Aerospace Sciences
, vol.25
, Issue.2
, pp. 54-67
-
-
Fay, J.A.1
Ridell, F.R.2
-
28
-
-
3943108178
-
-
NASA TM-104792, June
-
Williams, S. D., Curry, D. M., Chao, D., and Pham, V. T., "Analysis of the Shuttle Orbiter Reinforced Carbon-Carbon Oxidation Protection System," NASA TM-104792, June 1994.
-
(1994)
Analysis of the Shuttle Orbiter Reinforced Carbon-Carbon Oxidation Protection System
-
-
Williams, S.D.1
Curry, D.M.2
Chao, D.3
Pham, V.T.4
-
30
-
-
3943087006
-
-
NASA CDTM-20007, March
-
Stewart, D. A., Pallix, J., and Esfahani, L., "Surface Catalytic Efficiency of Candidate Ceramic Thermal Protection Materials for SSTO," NASA CDTM-20007, March 1995.
-
(1995)
Surface Catalytic Efficiency of Candidate Ceramic Thermal Protection Materials for SSTO
-
-
Stewart, D.A.1
Pallix, J.2
Esfahani, L.3
-
31
-
-
0038764433
-
-
NASA CP-2283, March
-
Stewart, D. A., Rakich, J. V, and Lanfranco, M. J., "Catalytic Surface Effects on Space Shuttle Thermal Protection System During Earth Entry of Flights STS-2 Through STS-5," NASA CP-2283, March 1983.
-
(1983)
Catalytic Surface Effects on Space Shuttle Thermal Protection System during Earth Entry of Flights STS-2 Through STS-5
-
-
Stewart, D.A.1
Rakich, J.V.2
Lanfranco, M.J.3
|