Analysis of forced response in a wind tunnel based on Doublet-Lattice method

Author:

Schmidt H.,Neumann J.,Mai H.

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference13 articles.

1. Hoblit, F.M.: Gust Loads on Aircraft: Concepts and Applications. AIAA Education Series, Washington (1988)

2. Federal Aviation Administration, Airworthiness standards: Transport category airplanes, FAA, 14 CFR Part 25 (2010)

3. European Aviation Safety Agency, Certification Specifications for Large Airplanes CS-25, ED Decision 2010/013/R (2010)

4. Rodden, W.P., Johnsen, E.H.: MSC/NASTRAN Aeroelastic Analysis User’s Guide, MSC. Software Corporation (2004)

5. ZONA Technology Inc.: ZAERO Version 8.4 Engineers Toolkit for Aeroelastic Analysis, Theoretical Manual, ZONA Technology Inc. (2008)

Cited by 2 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. Numerical Modeling of Wind Tunnel Walls for the Investigation of Oscillating Airfoils;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2016

2. Design and aeroelastic assessment of a forward-swept wing aircraft;CEAS Aeronautical Journal;2014-06-21

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