NPFC - MIL-A-8870
AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
inactive
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| Organization: | NPFC |
| Publication Date: | 20 May 1987 |
| Status: | inactive |
| Page Count: | 39 |
Document History
June 11, 2019
Airplane Strength and Rigidity Vibration, Flutter, and Divergence
A description is not available for this item.
August 12, 2014
Airplane Strength and Rigidity Vibration, Flutter, and Divergence
A description is not available for this item.
March 25, 1993
AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
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...
MIL-A-8870
May 20, 1987
AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
A description is not available for this item.
May 18, 1987
AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
A description is not available for this item.
March 31, 1971
AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
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,...
May 18, 1960
AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
General.-
This Specification contains the general requireprents for:
(a) Flutter, divergence, and vibration (including c m &ort) oharacteristics which shall be provided i n airplanes.
(b) Certain...