Orbiter entry leeside heat-transfer data analysis-Reference-Cited by-同舟云学术

Orbiter entry leeside heat-transfer data analysis

Published:1983-11 Issue:6 Volume:20 Page:524-530
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Throckmorton D. A.¹,Zoby E. V.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.8582

Reference16 articles.

1. Lee-surface vortex effects over configurations in hypersonic flow

2. 3Hefner, J. N. "Lee-Surface Heating and Flow Phenomena on Space Shuttle Orbiters at Large Angles of Attack and Hypersonic Speeds," NASA TN D-7088,1972.

3. Effect of Nose Geometry on the Aerothermodynamic Environment of Shuttle Entry Configurations

4. Hypersonic Lee Surface Flow Phenomena over a Space Shuttle

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