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MIL-A-8870C: AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
Abstract: This specification contains the general and detail design requirements and criteria in the design and construction of airplanes to:
a. Prevent flutter, divergence, and other dynamic and static aeroelastic instabilities. ...
a. Prevent flutter, divergence, and other dynamic and static aeroelastic instabilities. ...
MIL-M-8856B: MISSILES, GUIDED, STRUCTURAL INTEGRITY, GENERAL SPECIFICATION FOR
Abstract: This specification establishes the structural performance and verification requirements for guided missiles. The requirements of this specification are established to assure that guided missiles delivered to operational ...