Efficient vibration mode analysis of aircraft with multiple externalstore configurations

Author:

Karpel M.1

Affiliation:

1. Israel Aircraft Industries, Lod, Israel

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 29 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. Evaluation of Generalised Forces Using CFD-Based Methods for Efficient Linear/Nonlinear Simulations;AIAA SCITECH 2024 Forum;2024-01-04

2. Research on Dynamic Characteristics of Aircraft with Floating Material;2022 International Conference on Automation, Robotics and Computer Engineering (ICARCE);2022-12-16

3. Vibration analyses of an equivalent plate wing with an external store;The Aeronautical Journal;2014-09

4. Substructure synthesis method for a nonlinear structure with a sliding mode condition;Journal of Sound and Vibration;2009-04

5. The Structural Order Reduction Challenge in the Case of Geometrically Nonlinear Joined-Wing Confgurations;48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2007-04-23

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