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Local Piston Theory with Viscous Correction and Its Application

Published:2017-03 Issue:3 Volume:55 Page:942-954
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Liu Wen¹,Zhang Chen-An²,Han Han-Qiao³,Wang Fa-Min²

Affiliation:

1. Northwestern Polytechnical University, Xi’an 710072, People’s Republic of China

2. Chinese Academy of Sciences, Beijing 100190, People’s Republic of China

3. Wuhan Second Ship Design and Research Institute, Wuhan 430072, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J055207

Reference30 articles.

1. Unsteady aerodynamic and aeroelastic calculations for wings using Euler equations

2. Hypersonic and High-Temperature Gas Dynamics, Second Edition

3. Oscillating Airfoils at High Mach Number

4. Van DykeM. “A Study of Second-Order Supersonic Flow Theory,” NACA TR 1081, 1951.

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