A Sensitivity Study of Downwash Weighting Methods for Transonic Aeroelastic Stability Analysis-Reference-Cited by-同舟云学术

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A Sensitivity Study of Downwash Weighting Methods for Transonic Aeroelastic Stability Analysis

Published:2004-06-20 Issue: Volume: Page:
ISSN:
Container-title:22nd Applied Aerodynamics Conference and Exhibit
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Author:

Silva Roberto¹,Mello Olympio¹,Azevedo Joao¹

Affiliation:

1. Aerospace Technical Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-5375

Reference30 articles.

1. Role of Shocks in the "Sub-Transonic" Flutter Phenomenon

2. Lessing,H.C.,Troutman, J. L., and Menees, G. P."Experimental Determination on aRectangular WingOscillatinginthe First BendingModefor Mach Numbers from0.24 to 1.30,"NASATND-33, December 1960.

3. Isogai, K. "Numerical Simulation of Transonic Flutter of a High-Aspect-Ratio Transport Wing", National Aerospace Laboratory, Japan, Report TR-776T, August,1983.

Cited by 1 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. An Investigation on Viscous Effects in Downwash Weighting Methods for Transonic Aeroelastic Stability Analysis;23rd AIAA Applied Aerodynamics Conference;2005-06-06

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