NPFC - MIL-A-8870
AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
| Organization: | NPFC |
| Publication Date: | 31 March 1971 |
| Status: | inactive |
| Page Count: | 20 |
scope:
This specification contains the general requirements for:
a. Prevention of flutter, divergence, and other aeroelastic instabilities in the designing and construction of airplanes
b. Analyses, flight tests, and ground tests to assure freedom from flutter, divergence, and other aeroelastic instabilities of airplanes.
intended Use:
The requirements of this specification are intended for use in the design and substantiation of airplanes from the specified structural, dynamic, and aeroelastic viewpoints.
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