Approximate Heating Analysis for the Windward Symmetry Plane of Shuttle-like Bodies at Large Angle of Attack-Reference-Cited by-同舟云学术

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Approximate Heating Analysis for the Windward Symmetry Plane of Shuttle-like Bodies at Large Angle of Attack

Published:1982-01-01 Issue: Volume: Page:229-247
ISSN:
Container-title:Thermophysics of Atmospheric Entry
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Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/5.9781600865565.0229.0247

Reference46 articles.

1. ^artindale, W. R. "Test Results from NASA Rockwell International Space Shuttle Test (OH4B) Conducted in the AEDC-VKF Tunnel B," AEDC-DR-74-8, Jan.1974.

2. 2Dye, W. H. "Results of Heat Transfer Test of a 0.0175-Scale Space Shuttle Orbiter 104BModel (Modified 22-0)in the NASA/Ames Research Center 3.5-Foot Hypersonic Wind Tunnel (Test }H26],UNASA CR-151380, Oct. 1977.

3. 3Harthun, M. H. "Orbiter Entry Heating Analysis-OCR Report," Rockwell International, Rept. SAS-AAT-79-048, Feb.1979.

4. 4"SpaceTransportationSystemTechnologySymposium,Vol.I:Aero-thermodynamics and Configurations," NASA TM X-52876, July 197Q.

5. Engineering flowfields and heating rates for highly swept wing leading edges

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A review of some approximate methods used in aerodynamic heating analyses;20th Thermophysics Conference;1985-06-19

2. Application of axisymmetric analogue for calculating heating in three-dimensional flows;23rd Aerospace Sciences Meeting;1985-01-14

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