Waveriders with finlets-Reference-Cited by-同舟云学术

Waveriders with finlets

Published:1994-09 Issue:5 Volume:31 Page:1135-1142
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

He X.¹,Rasmussen M. L.¹,Cox R. A.¹

Affiliation:

1. University of Oklahoma, Norman, Oklahoma 73019

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.46623

Reference7 articles.

1. Delta Wings of Shapes Amenable to Exact Shock-wave Theory

2. Waverider Configurations Derived from Inclined Circular and Elliptic Cones

3. 4He, X. "Computational Analysis of Hypersonic Flows Past Generalized Cone-Derived Waveriders," Ph.D. Dissertation, School of Aerospace and Mechanical Engineering,Univ. of Oklahoma, Norman,OK, 1992.

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4. Experimental verification of the osculating cones method for two waverider forebodies at Mach 4 and 6;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12

5. Effects of anhedral and finlets on lateral stability of hypersonic waveriders;35th Aerospace Sciences Meeting and Exhibit;1997-01-06