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Flutter Analysis of an F-16A/B in Heavy Store Configuration

  • Published:2005-11 Issue:6 Volume:42 Page:1565-1574
  • ISSN:0021-8669
  • Container-title:Journal of Aircraft
  • language:en
  • Short-container-title:Journal of Aircraft

Author:

Bennani Samir1,Beuker Bert2,van Staveren Jan Willem3,Meijer Jos J.4

Affiliation:

1. Delft University of Technology, Kluyverweg 1, 2629 HS, Delft, The Netherlands

2. Royal Netherlands National Air Force, Binkhorstlaan 135, 2516 BA, The Hague, The Netherlands

3. ADSE Consultancy and Engineering Services, Saturnusstraat 12, 2130 KB, Hoofddorp, The Netherlands

4. National Aerospace Research Laboratory, Anthony Fokkerweg 2, 1059 CM, Amsterdam, The Netherlands

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 11 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. Review on Flight Control Law Technologies of Fighter Jets for Flying Qualities;International Journal of Aeronautical and Space Sciences;2022-12-31

2. Linear Fractional Transformation co-modeling of high-order aeroelastic systems for robust flutter analysis;European Journal of Control;2020-07

3. Study of Flexible Aircraft Body Freedom Flutter with Robustness Tools;Journal of Guidance, Control, and Dynamics;2018-05

4. LPV modeling of a flexible wing aircraft using modal alignment and adaptive gridding methods;Aerospace Science and Technology;2017-07

5. LPV Model Development for a Flexible Wing Aircraft;58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2017-01-05
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