EFFECT OF VERTICLE-TAIL MODIFICATIONS ON THE STATIC STABILITY CHARACTERISTICS AT A MACH NUMBER OF 2.2 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS
By: Robinson,Ross B.
Contributor(s): Spearman,M Leroy.
Material type:
BookPublisher: Nasa, Washington, D.C. 1961Description: 17.DDC classification: NASA | TM X-519
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA TM X-519 (Browse shelf) | Not for loan | TR14307 |
Total holds: 0
Bound With Nasa Tm X-507-18,522-81, Lack No.509-13,515-17,519-21,523-29,531-39,541-46,548-65,567-68,572-80
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