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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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Transonic Flutter Characteristics Of A 45 Degree Swept Back All Movable Stabilizer
Author(s): D'Ewart, Benjamin B., Jr., Farrell, Robert F.
Corporate Author(s): Bell Aerospace Co Buffalo Ny
Laboratory: Aircraft Laboratory
Date of Publication: 1958-05
Report number: WADC TR 57-392

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