Transonic-Small-Disturbance and Linear Analyses for the Active Aeroelastic Wing Program-Reference-Cited by-同舟云学术

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Transonic-Small-Disturbance and Linear Analyses for the Active Aeroelastic Wing Program

Published:2005-04-18 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
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Author:

Wieseman Carol¹,Silva Walt¹,Spain Charles¹,Heeg Jennifer¹

Affiliation:

1. NASA Langley

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1995

Reference8 articles.

1. Efficient algorithm for solution of the unsteady transonic small-disturbance equation

2. Rodden, William P. and Johnson, Erwin H. :MSC/NASTRAN Aeroelastic Analysis Users Guide, Version 68, October 1994, The MacNeal-Schwendler Corporation.

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. Unique Testing Capabilities of the NASA Langley Transonic Dynamics Tunnel, an Exercise in Aeroelastic Scaling;AIAA Ground Testing Conference;2013-06-22

2. Control surface interaction effects of the Active Aeroelastic Wing wind tunnel model;47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th;2006-05

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