WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEED OF THE STATIC LONGITUDINAL STABILITY CHARACTERISTICS OF A WINGED REENTRY VEHICLE HAVING A LARGE NEGATIVELY DEFLECTED FLAP-TYPE CONTROL SURFACE
By: Fournier,Paul G.
Material type:
BookPublisher: Nasa, Washington, D.C. 1959Description: 21.DDC classification: NASA | TM X-179 -
| 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-179 - (Browse shelf) | Not for loan Untraceable | TR8836 |
Total holds: 0
Bound With Nasa Tm X-165-79
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