Comment on "An Empirical Expression for Drag Coefficients Cones at Supersonic Speeds"
Author:
Affiliation:
1. Lockheed Missiles & Space Company, Sunnyvale, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.55473
Reference11 articles.
1. APPROXIMATIONS FOR SUPERSONIC FLOW OVER CONES
Cited by 5 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. Analysis on the effect of hypersonic vehicle’s optical window on infrared thermal imaging system;SPIE Proceedings;2015-08-07
2. Blunt cone pressure correlations for supersonic and hypersonic flow;14th Applied Aerodynamics Conference;1996-06-17
3. A pressure formula for an inclined circular cone in supersonic flow,gamma = 1.4.;AIAA Journal;1972-02
4. Erratum: "Comment on 'An Empirical Expression for Drag Coefficients of Cones at Supersonic Speeds' ";AIAA Journal;1969-11
5. Errata: "Doublet-Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows";AIAA Journal;1969-11
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