Shock Location Dominated Transonic Flight Loads on the Active Aeroelastic Wing
Author:
Affiliation:
1. NASA Dryden Flight Research Center
2. U.S. Air Force Research Laboratory
3. Spiral Technologies, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-6315
Reference15 articles.
1. 2Miller,G.D."AnActiveFlexibleWingMulti-DisciplinaryDesignOptimizationMethod,"AIAA-94-4412-CP,1994.
2. 3Yurkovich,R."OptimumWingShapeforanActiveFlexibleWing,"AIAA-95-1220-CP,1995.
3. 4Pendleton, E., Griffin, K. E., Kehoe, M. W., and Perry, B. "A Flight Research Program for Active Aeroelastic Wing Technology," AIAA-96-1574-CP,1996.
4. Active Aeroelastic Wing Flight Research Program: Technical Program and Model Analytical Development
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1. Static Aeroelastic and Open-Loop Aeroservoelastic Analyses for the F/A-18 AAW Aircraft;48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2007-04-23
2. The X-53 A Summary of the Active Aeroelastic Wing Flight Research Program;48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2007-04-23
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