A NUMERICAL METHOD FOR DETERMINING THE AEROELASTIC DIVERGENCE CHARACTERISTICS OF UNGUIDED, SLENDER-BODY, MULTISTAGE LAUNCH VEHICLES
By: Young,Clarence P.
Material type:
BookPublisher: Nasa, Washington, D.C. 1967Description: 47.DDC classification: NASA | TN D-3893
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA TN D-3893 (Browse shelf) | Not for loan | TR10425 |
Total holds: 0
Bound With Nasa Tn D-3891, 92 And D-3894-3900
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