Oscillating Airfoils at High Mach Number-Reference-Cited by-同舟云学术

Oscillating Airfoils at High Mach Number

Published:1953-06 Issue:6 Volume:20 Page:402-406
ISSN:1936-9956
Container-title:Journal of the Aeronautical Sciences
language:en
Short-container-title:Journal of the Aeronautical Sciences

Author:

LIGHTHILL M. J.¹

Affiliation:

1. University of Manchester, England

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.2657

Reference4 articles.

1. Hayes, W. D., Q. App. Math., Vol. 5, pp. 105-106, 1947.

2. Goldsworthy, F. A., Q.J.M.A.M., Vol. 5, pp. 54-63, 1952.

3. Jones, W. P., The Influence of Thickness-Chord Ratio on Supersonic Derivatives for Oscillating Aerofoils, A.R.C. Report 10871 (limited circulation), to be published as A.R.C. R. & M. 2679.

Cited by 247 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. Effect of Model Fidelity on High-Speed Aeroelastic Behavior of a Cantilever Plate;AIAA Journal;2024-08-05

2. Numerical investigation of fluid-thermal-structural interaction of deployable control fin in hypersonic flow;Physics of Fluids;2024-08-01

3. Thermo-aeroelastic analysis of triangular composite plate with embedded shape memory alloy at supersonic flow;Journal of Intelligent Material Systems and Structures;2024-07-24

4. Exact Eigensolutions of Two-Dimensional Laminated Panel Flutter Based on Mindlin Plate Theory and the First-Order Piston Theory;International Journal of Structural Stability and Dynamics;2024-06-01

5. Approximate global mode method for flutter analysis of folding wings;International Journal of Mechanical Sciences;2024-03