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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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