Transonic Flutter Characteristics of an Arrow Wing Mounted with Engine-Reference-Cited by-同舟云学术

Transonic Flutter Characteristics of an Arrow Wing Mounted with Engine

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Machida Shigeru¹,Kikuchi Takao¹,Arizono Hitoshi¹,Saitoh Kenichi¹,Nakamichi Jiro¹

Affiliation:

1. Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-835

Reference6 articles.

1. 2Saitoh, K., Kikuchi, T., and Tamayama, M. "Wind Tunnel Flutter Tests for NEXST-1," International Forum on Aeroelasticityand StructuralDynamics2003,Amsterdam,June2003.

2. 3Nakamichi,J.,Saitoh,K.,andHamidReza,K."Numerical AeroelasticityTestingand Assement Systemdeveloped atNAL ofJapan,"InternationalForumon Aeroelasticityand StructuralDynamics2003,Amsterdam,June2003.

3. 4DowellE.,Edwards,J.,andStrganac,T.W. "NONLINEARAEROELASTICITY,"AIAAPaper2003-1816,April2003.

4. 5Edwards, J. W., Schuster D. M., Spain, C. V., Keller, D. F., and Moses, R. W. "MAVRIC Flutter Model Transonic Limit CycleOscillation Test,"NASATM-2001-210877,May2001.

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