Modified-strip-analysis method for predicting wing flutter at subsonic to hypersonic speeds.-Reference-Cited by-同舟云学术

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Modified-strip-analysis method for predicting wing flutter at subsonic to hypersonic speeds.

Published:1966-01 Issue:1 Volume:3 Page:25-29
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

YATES E. CARSON¹

Affiliation:

1. NASA Langley Research Center, Hampton, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.43702

Reference20 articles.

1. Theodorsen, T. "General theory of aerodynamic instability and the mechanism of flutter/' NACA Rept. 496 (1935).

2. Smilg, B. and Wassermaii, L. S. "Application of three-dimensional flutter theory to aircraft structure/' Air Corps Technical Rept. 4798, Material Div., Army Air Corps (July 9, 1942).

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