Effects of structural nonlinearities on limit cycle response of aerodynamic surfaces-Reference-Cited by-同舟云学术

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Effects of structural nonlinearities on limit cycle response of aerodynamic surfaces

Published:1986-05-19 Issue: Volume: Page:
ISSN:
Container-title:27th Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

LAURENSON R.¹,HAUENSTEIN A.¹,GUBSER J.¹,BRILEY R.²

Affiliation:

1. McDonnell Douglas Astronautics Co., St. Louis, MO

2. Harris Corp., Melbourne, FL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-899

Reference28 articles.

1. 3539. October 1955.

2. Aeronautical Sciences, Vol. 24, January 1957,

3. pp. 57-63.

4. Aerospace Science, Vol. 26. January 1959, pp.

5. 25-32, 45.

Cited by 6 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. Control-Surface Structural Nonlinearities in Aeroelasticity: A State of the Art Review;AIAA Journal;2022-06

2. An investigation of stability of a control surface with structural nonlinearities in supersonic flow using Zubov's method;Journal of Sound and Vibration;2009-08

3. Nonlinear Stability Analysis of Control Surface Flutter with Freeplay Effects;Journal of Aircraft;2008-11

4. AN INVESTIGATION OF STABILITY IN THE LARGE BEHAVIOUR OF A CONTROL SURFACE WITH STRUCTURAL NON-LINEARITIES IN SUPERSONIC FLOW;Journal of Sound and Vibration;2002-09

5. Limit cycle phenomena in computational transonic aeroelasticity;Journal of Aircraft;1994-11

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