F-16 Wing Structural Deflection Testing - Phase I
Author:
Affiliation:
1. U.S. Air Force
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1674
Reference3 articles.
1. Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores
2. Patil,MayureshJ.,Hodges,DeweyH.,andCesnik,CarlosE.S."NonlinearAeroelasticityandFlightDynamicsofHigh-Altitude Long-Endurance Aircraft,"40thStructures,StructuralDynamicsandMaterialsConference,AIAA99-1470,St.Louis, Missouri, April12-15, 1999.
3. Lokos,WilliamA.,Olney,CandidaD.,Crawford,NatalieD.,Stauf,Rick,andReichenback,EricY."WingTorsional Stiffness Tests of the Active Aeroelastic WingF/A-18 Airplane,"NASA/TM-2002-210723, May2002.
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