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Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 1: Model Design And Testing Techniques
Author(s): McCarthy, John F., Jr., Prigge, John S., Jr., Levy, Gilbert M., Asher, Gifford W.Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report number: WADC TR 54-113 Part 1
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Supersonic Flutter Trends As Revealed By Piston Theory Calculations
Author(s): Ashley, Holt, Zartarian, GarabedCorporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-05
Report number: WADC TR 58-74
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Gust Loading Of Rigid And Flexible Aircraft In Continous Atmospheric Turbulence
Author(s): Foss, Kenneth A., McCabe, Warren L.Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-01
Report number: WADC TR 57-704
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Unsteady Airloads On Pointed Airfoils And Slender Bodies At High Mach Numbers
Author(s): Zartarian, GarabedCorporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1959-12
Report number: WADC TR 59-583
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