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Vibration Analysis of a Cantlievered Square Plate by the Stiffness Matrix Method
Author(s): Best, G. C.Corporate Author(s): General Dynamics
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-11
Report number: AFFDL-TR-66-80 p. 849-860
full text available
Design, Development, and Flight Test of Multiplexing Hardware for Use in a Fly-by-Wire Flight Control System
Author(s): Mrazek, J. G., Roberts, R. O.Corporate Author(s): General Dynamics
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-43
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