Maximum Control Surface Freeplay, Design and Flight Testing Approach on the F-22-Reference-Cited by-同舟云学术

Maximum Control Surface Freeplay, Design and Flight Testing Approach on the F-22

Published:2007-04-23 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

Anderson William¹,Mortara Sean²

Affiliation:

1. Lockheed Martin Aeronautics Company

2. U.S. Air Force

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1767

Reference5 articles.

1. 3JointServiceSpecificationGuide2006,Wright-PattersonAFB,OH,1998.

2. 4Guruswamy, G. P., and Byun, C. "Fluid-Structural Interactions Using Navier-Stokes Flow Equations Coupled with Shell FiniteElement Structures", AIAA-93-3087.

3. 5Anderson,W.D.,TransonicBuzz-W/TTestandENSAEROAnalysisComparison,AerospaceFlutter&DynamicsCouncil, Monterey, CA, 9-10 Oct, 2003.

Cited by 15 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. Wind Tunnel Tests of an Aeroelastic Model with Multiple Control Surface Freeplay Nonlinearities;AIAA SCITECH 2024 Forum;2024-01-04

2. Experimental and numerical flutter analysis of a folding fin with multiple asymmetric free-plays;Chinese Journal of Aeronautics;2023-11

3. Study of Nonlinear Stiffness and Damping Effects on Shimmy and Flutter;Journal of Aircraft;2023-11

4. A new look at the Equivalent Linearization Technique to predict LCO in aeroelastic systems with discrete nonlinearities;Journal of Fluids and Structures;2023-05

5. Nonlinear Dynamics of an All-Movable Rudder System with Freeplay Nonlinearity;Iranian Journal of Science and Technology, Transactions of Mechanical Engineering;2023-03-04