Development of Generalized Aeroservoelastic Reduced Order Models-Reference-Cited by-同舟云学术

Development of Generalized Aeroservoelastic Reduced Order Models

Published:2009-05-04 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Roughen Kevin¹,Bendiksen Oddvar²,Baker Myles¹

Affiliation:

1. M4 Engineering, Inc.

2. University of California, Los Angeles

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2491

Reference26 articles.

1. 1Baker, M. L. and Lenkey, P. W. Parametric Flutter Analysis of the TCA Configuration and Recommendation for FFM Design and Scaling,McDonnell Douglas Report CRAD-9306-TR-3088

2. 2Fogarty, T., and Baker, M. L. MSC/NASTRAN Flutter Analysis of TCA with Lateral and Directional Control Laws, 6/30/1998.HSRProgram memorandum

3. Transonic aeroelastic analysis of a high speed transport wind tunnel model

4. Role of shock dynamics in transonic flutter

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1. Optimization of High Altitude Long Endurance (HALE) Vehicle Subject to Flutter Speed Constraint;57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2016-01-01

2. An Overview of the Semi-Span Super-Sonic Transport (S4T) Wind-Tunnel Model Program;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 20th AIAA/ASME/AHS Adaptive Structures Conference 14th AIAA;2012-04-23

3. Generation of Aeroservoelastic Reduced Order Models Using Time Scaling;51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 18th AIAA/ASME/AHS Adaptive Structures Conference 12th;2010-04-12

4. Active Flutter Suppression of the Supersonic Semispan Transport (S4T) Model;51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 18th AIAA/ASME/AHS Adaptive Structures Conference 12th;2010-04-12