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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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The Computation of Dynamic Response Time Histories of a System Using a Matrix Iterative Technique
Author(s): D'Ewart, Benjamin B., Jr., Farrel, Robert F.
Corporate Author(s): Bell Aerosystems Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-11
Report number: AFFDL-TR-66-80 p. 727-742

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