Aerodynamics of a simple cone-derived waverider-Reference-Cited by-同舟云学术

Aerodynamics of a simple cone-derived waverider

Published:1984-01-09 Issue: Volume: Page:
ISSN:
Container-title:22nd Aerospace Sciences Meeting
language:
Short-container-title:

Author:

BROADAWAY ¹

Affiliation:

1. Oklahoma, University, Norman, OK

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1984-85

Reference7 articles.

1. D. Kiichemann (1978), '"The Aerodynamic i)esign of Aircraft, Perganon Press, London, pp.44R-510.

2. .I. R. Collingbourne and D. H. Peckhnm (19h7), "The Lift and Drag Characteristics of Carct Wings nt. Mach Numbers Between 5 and Ifl,'' A.R.C. C.1'. NO. 930. 1.I. 6. Jones (19631, "A Nethod for Designing ILifting Configurntions for High Supersonic Speeds Using the Flow Ficlrls of Yon-Lifting Cones," lN.4.E. Rcimrt No. tkro 2674, A.R.C 24846.

3. Waverider Configurations Derived from Inclined Circular and Elliptic Cones

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3. Heat Transfer Measurements On Waverider at Hypersonic Mach Numbers;19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2014-06-13

4. Comparison between Methods of Generation of Waveriders Derived from Streamline Tracing and Simplified Method;Applied Mechanics and Materials;2013-08

5. Shock tunnel testing of a Mach 6 hypersonic waverider;Shock Waves;2009