THE STATIC AND DYNAMIC ROTARY STABILITY DERIVATIVES AT SUBSONIC SPEEDS ON AN AIRPLANE MODEL HAVING WING AND TAIL SURFACES SWEPT BACK 45
By: Lopez,Armando E,Buell,Donald A.
Contributor(s): Tinling,Bruce E.
Material type:
BookPublisher: Nasa, Washington, D.C. 1959Description: 75.DDC classification: NASA | MEMO 5-16-59A
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA MEMO 5-16-59A (Browse shelf) | Not for loan | TR11440 |
Total holds: 0
Bound With Nasa Memo 5-12-59a,5-18-59a-5-20-59a Lack No. 13-15,17,19
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