MIL A 008870 : A
Superseded
View Superseded by
AIRPLANE STRENGTH AND RIGIDITY FLUTTER, DIVERGENCE AND OTHER AEROELASTIC INSTABILITIES
07-23-2013
Covers prevention of flutter, divergence and other aeroelastic instabilities in the designing and construction of airplanes. Analyses, flight tests and ground tests.
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-M-81260 Revision A:1971 | Manual, Technical, Aircraft/System/Equipment Maintenance |
| MIL-A-8868 Revision B:1987 | Airplane Strength and Rigidity Data and Reports (No S/S Document) |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
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