Numerical Computation of Space Shuttle Laminar Heating and Surface Streamlines-Reference-Cited by-同舟云学术

Numerical Computation of Space Shuttle Laminar Heating and Surface Streamlines

Published:1977-05 Issue:5 Volume:14 Page:265-272
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Rakich John V.¹,Lanfranco Martin J.²

Affiliation:

1. NASA Antes Research Center, Moffett Field, Calif.

2. Informatics, Inc., Palo Alto, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.57192

Reference21 articles.

1. 'Rakich, J. V. and Park, C. "Nonequilibrium Three-Dimensional Supersonic Flow Computations with Application to the Space Shuttle Orbiter Design,'* Proceedings of the Symposium on Application of Computers to Fluid Dynamic Analysis and Design, Polytechnic Institute of Brooklyn Graduate Center, Farmingdale, N. Y., Jan. 1973.

2. 2Rizzi, A. and Bailey, H. "Reacting Nonequilibrium Flow Around the Space Shuttle Using a Time Split Method," NASA SP 347,1975.

3. Computation of nonequilibrium three-dimensional inviscid flow over blunt-nosed bodies flying at supersonic speeds

4. Computational procedure for evaluation of space shuttle TPS requirements

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