1 |
Shapiro, A., H., The Dynamics and Thermodynamics of Compressible Fluid Flow, Wiley, New York, 1953.
|
2 |
Glass, C., E., Holden, M., S., and Wieting, A., R., "Effect of Leading Edge Sweep on Shock/Shock Interference at Mach 8", AIAA Paper 89-0271, Reno, NV, 1989.
|
3 |
Reubush, D., E., and Omar, M., E., "Pressure and Heat Transfer Investigation of a Modified NASP Baseline Configuration at M=6", AIAA Paper 89-0246, Reno, NV, 1989.
|
4 |
Fujimoto, K., Fujii, K., and Tsuboi, N., "CFD Prediction of the Aerodynamic Characteristics of Capsulelike Configurations for the Future SSTO Development", 41st AIAA Aerospace Science Meeting, AIAA Paper 03-0912, Reno, NV, 2003.
|
5 |
Galkin V., S., Erofeev A., I., and Tolstykh A., I., "Approximate method of calculation of the aerodynamic characteristics of bodies in a hypersonic rarefied gas", Proceedings of TsAGI, Issue No. 1833, 1977, pp. 6-10. (in Russian)
|
6 |
Zay Yar Myo Myint, and Khlopkov, A., Yu., "Aerodynamic Characteristics of an Aircraft with a Complex Shape Taking into Account the Potential of Molecular Flow Interaction with a Surface", TsAGI Science Journal, Vol. 41, No. 5, 2010, pp. 551-566. DOI: 10.1615/TsAGISciJ.v41.i5.50
DOI
|
7 |
Vaganov, A., V., Drozdov, S., Kosykh, A., P., Nersesov, G., G., Chelysheva, I., F., and Yumashev, V., L., "Numerical Simulation of Aerodynamics of Winged Reentry Space Vehicle", TsAGI Science Journal, Vol. 40, No. 2, 2009, pp. 131-149. DOI:10.1615/TsAGISciJ.v40.i2.10
DOI
|
8 |
Kogan, N., M., Rarefied Gas Dynamic, Plenum, New York, 1969.
|
9 |
Belotserkovskii, O., M., and Khlopkov, Y., I., Monte Carlo Methods in Mechanics of Fluid and Gas, World Scientific Publishing Co., N-Y, London, Singapore, Beijing, Hong Kong, 2010.
|
10 |
Moss, J., N., Glass, C., G., Hollis, B., R., and Van, Norman, J., W., "Low Density Aerothermodynamics of the Inflatable Reentry Vehicle Experiment", AIAA Paper 2006-1189, 2006.
|
11 |
Horvath, T., J., Berry, S., A., and Merski, N., R., "Hypersonic Boundary/Shear Layer Transition for Blunt to Slender Configurations - A NASA Langley Experimental Perspective", Enhancement of NATO Military Flight Vehicle Performance, Czech Republic, 4-7 October 2004, RTO-MPAVT-111.
|
12 |
Ivanov, M., S., "Statistical Simulation of Reentry capsule Aerodynamics in Hypersonic Near-Continuum Flows", RTO lecture series, Models and Computational Methods for Rarefied Flows EN-AVT-194-18, (AVT-194), 2011.
|
13 |
Neumann, R., D., "Missions and requirements. Special Course Aerothermodynamics of Hypersonic Vehicles", AGARD Report 761, Neuilly sur Seine, France, 1988.
|
14 |
Hirschel, E., H., Basics of Aerothermodynamics, Springer-Verlag, Berlin, Heidelberg, New York, 2005.
|
15 |
Bird, G., A., Molecular Gas Dynamics and the Direct Simulation of Gas Flows, Oxford University Press, New York, 1994.
|
16 |
Anderson, J., D., Hypersonic and High-Temperature Gas Dynamics, McGraw-Hill, New York, 1988.
|
17 |
Lees, L., "Hypersonic Flow", Processing of 5th International Aeronautical Conference, Los Angeles, New York, 1955, pp. 241-275.
|
18 |
Bertin, J., J., and Cummings, R., M., "Critical Hypersonic Aerothermodynamic Phenomena", Annual Review of Fluid Mechanics, Vol. 38, 2006, pp. 129-157. DOI: 10.1146/annurev.fluid.38.050304.092041
DOI
ScienceOn
|