The shapes of bodies with maximum lift-to-drag ratio in supersonic flow-Reference-Cited by-同舟云学术

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The shapes of bodies with maximum lift-to-drag ratio in supersonic flow

Published:2009-01 Issue:5 Volume:73 Page:514-523
ISSN:0021-8928
Container-title:Journal of Applied Mathematics and Mechanics
language:en
Short-container-title:Journal of Applied Mathematics and Mechanics

Author:

Lapygin V.I.,Yakunina G.Ye.

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials,Modeling and Simulation

Reference13 articles.

1. Gas Flows with a High Supersonic Velocity;Chernyi,1959

2. Trade-off of aerodynamic configuration for a descrete vehicle;Lapygin,2007

3. Theory of Optimum Aerodynamic Shapes Ed. by A. Miele. New York.: Acad. Press, 1965.

4. A wing with maximum lift-to-drag ratio at hypersonic velocities;Maikapar;Prikl Mat Mekh,1966

5. Maximum lift-to-drag ratio of a slender, flat-top, hypersonic body;Miele;Astronaut. Acta.,1967

Cited by 1 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. Simulation of Flows Near Wings with Supersonic Edges;Advances in Theory and Practice of Computational Mechanics;2022

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