Incorrectness of the k Method for Flutter Calculations

Author:

Patil Mayuresh J.1,Yurkovich Rudolph N.2,Hodges Dewey H.3

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

2. The Boeing Company, St. Louis, Missouri 63166

3. Georgia Institute of Technology, Atlanta, Georgia 30332-0150

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 9 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. Flutter Calculation Methods;Introduction to Aeroelasticity;2023

2. Uncertainty quantification of aeroelastic wings flutter using an optimized machine learning approach;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-04-23

3. Investigation of Shock Motion in Transonic Flow Using an Oscillating, Straked, Delta Wing;AIAA Journal;2019-10

4. Flutter analysis of a viscoelastic tapered wing under bending–torsion loading;Meccanica;2018-11-01

5. Nonlinear Geometric Effects on Aero-viscoelasticity;2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2018-01-07

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