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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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Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part II. Experimental And Theoretical Data For Bare wings And wings with Tip Tanks
Author(s): McCarthy, John F., Jr., Martuccelli, John R., Asher, Gifford W., Zartarian, Garabed
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report number: WADC TR 54-113 Part 2
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Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 3: Experimental and Theoretical Data for Wings with Control Surfaces
Author(s): Asher, Gifford W., Weatherhill, Warren H.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-01
Report number: WADC TR 54-113 Part 3
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Flutter Model Tests Of A Swept-back, All-moving Horizontal Tail At Supersonic Speeds
Author(s): Asher, Gifford W.
Corporate Author(s): Massachusetts Inst Of Tech Cambridge
Laboratory: Aircraft Laboratory
Date of Publication: 1957-11
Report number: WADC TR 56-285
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Admittance Techniques In high Speed Flutter Model Testing. Part I. Experimental Results
Author(s): Asher, Gifford W., Watanabe, Roy K.
Corporate Author(s): Boeing Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-07
Report number: WADD TR 61-31 Part I

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