A Second-Order Solution for an Oscillating Two-Dimensional Supersonic Airfoil
Author:
Affiliation:
1. The RAND Corporation,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.2430
Reference22 articles.
Cited by 5 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. Data-Driven Unsteady Aerodynamic Modeling for Studying Subsonic Fluid-Structure Interaction;AIAA AVIATION 2023 Forum;2023-06-08
2. Aerodynamische Grundlagen;Grundlagen der Aeroelastik;1974
3. The Effect of Thickness on Airfoils with Constant Vertical Acceleration at Supersonic Speeds;Journal of the Aeronautical Sciences;1955-03
4. A Method for Location of Detached Shock Waves Ahead of Plane Bodies;Journal of the Aeronautical Sciences;1953-01
5. On Second-Order Supersonic Flow Past a Slowly Oscillating Airfoil;Journal of the Aeronautical Sciences;1953-01
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