Minimum Drag Power-Law Shapes for Rarefied Flow-Reference-Cited by-同舟云学术

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Minimum Drag Power-Law Shapes for Rarefied Flow

Published:2002-05 Issue:5 Volume:40 Page:1013-1015
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Bowman D. S.¹,Lewis Mark J.¹

Affiliation:

1. University of Maryland, College Park, Maryland 20742

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.1743

Reference6 articles.

1. Optimum Nose Shapes for Missiles in the Superaerodynamic Region

2. Bird, G. A., Molecular Gas Dynamics and the Direct Simulation of Gas Flows, Clarendon, New York, 1994, pp.1-14.

3. Goodman, F. O., and Wachman, H. Y., Dynamics of Gas-Surface Scattering, Academic Press, New York, 1976, pp.23, 24.

Cited by 3 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. Attitude Stabilization of Spacecraft in Very Low Earth Orbit by Center-Of-Mass Shifting;Frontiers in Robotics and AI;2019-02-14

2. Blunted-Cone Heat Shields of Atmospheric Entry Vehicles;AIAA Journal;2009-07

3. Minimum forebody drag in hypersonic continuum and rarefied flows;The Aeronautical Journal;2006-06

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