F-22 Aeroelastic Design and Test Validation
Author:
Affiliation:
1. Lockheed Martin Aeronautics Company
2. U.S. Air Force
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1764
Reference12 articles.
1. 2AircraftStructures,GeneralSpecificationfor,AFGS-87221A,8June1990.
2. 3F-22AirVehicleStructuralDesignCriteriaReport,F-22ProgramReport5PPYA005K,May2005.
3. An approximate true damping solution of the flutter equation by determinant iteration.
4. Application of the Doublet-Lattice Method to Nonplanar Configurations in Subsonic Flow
5. A harmonic gradient method for unsteady supersonic flow calculations
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