Hypersonic Pressure, Skin-Friction and Heat Transfer Distributions On Space Vehicles: Three-Dimensional Bodies-Reference-Cited by-同舟云学术

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Hypersonic Pressure, Skin-Friction and Heat Transfer Distributions On Space Vehicles: Three-Dimensional Bodies

Published:2004-10 Issue:10 Volume:42 Page:2070-2081
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Jain Amolak C.¹,Hayes James R.²

Affiliation:

1. Science and Technology Corporation, Hampton, Virginia 23666

2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.4104

Reference29 articles.

1. Hypersonic Pressure, Skin-Friction, and Heat Transfer Distributions On Space Vehicles: Planar Bodies

2. 2Weatherburn, C. E., Differential Geometry of Three Dimensions, Cambridge Univ. Press, London, 1964, pp.66-78.

3. Engineering flowfield method with angle-of-attack applications

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1. Engineering model for heat transfer to a complex-geometry deployable heat shield;AIAA Scitech 2021 Forum;2021-01-04

2. Effect of Environment Parameters on the Ablation of Hypersonic Missile Wing;Journal of Spacecraft and Rockets;2020-01

3. Asymptotic investigation of heat transfer and skin friction in three-dimensional hypersonic rarefied gas flows;Journal of Applied Mathematics and Mechanics;2016

4. Heat transfer—A review of 2004 literature;International Journal of Heat and Mass Transfer;2010-10

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