Structural Dynamics and Quasistatic Aeroelastic Equations of Motion-Reference-Cited by-同舟云学术

Structural Dynamics and Quasistatic Aeroelastic Equations of Motion

Published:2000-05 Issue:3 Volume:37 Page:538-542
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Dykman John R.¹,Rodden William P.¹

Affiliation:

1. The Boeing Company, Long Beach, California 90807-5309

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.2634

Reference11 articles.

1. Helicopter Inverse Simulation Incorporating an Individual Blade Rotor Model

2. Generalized technique for inverse simulation applied to aircraft maneuvers

3. 4Rutherford, S. “Simulation Techniques for the Study of the Manoeuvring of Advanced Rotorcraft Configurations,” Ph.D. Dissertation, Dept. of Aerospace Engineering,Univ. of Glasgow, Glasgow, Scotland, U.K.March 1997.

4. Equations of motion of an elastic flight vehicle utilizing static aeroelastic characteristics of the restrained vehicle

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