Supersonic and Hypersonic Minimum Drag for Bodies of Revolution-Reference-Cited by-同舟云学术

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Supersonic and Hypersonic Minimum Drag for Bodies of Revolution

Published:2003-06-21 Issue: Volume: Page:
ISSN:
Container-title:21st AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Auman Lamar¹,Wilks Brett¹

Affiliation:

1. U.S. Army Aviation and Missile Command

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-3417

Reference23 articles.

1. Seiff, Sandahl, Chapman, Perkins, Gowen, "Aerodynamic Characteristics of Bodies at Supersonic Speeds - A collection of three papers", NACA RM A51J25, November 1951.

2. Perkins, Jorgensen, "Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach numbers from 1.24 to 3.67", NACA RM A52H28, January1951.

3. Eggers, Resnikoff, Dennis, "Bodies of Revolution having Minimum Drag at High Supersonic Airspeeds", NACA Report 1306, 1957.

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