EFFECTS OF ROUNDING CORNERS AND LEADING EDGES ON THE WINDWARD-SURFACE PRESSURE OF A DELTA WING SWEPT 65(DG) AT A MACH NUMBER OF 5.96 AT ANGLES OF ATTACK FROM 65(DG) TO 115(DG)AND ANGLES OF ROLL FROM..
By: Goldberg,Theodore J.
Contributor(s): Blanchard,Doris K.
Material type:
BookPublisher: Nasa, Washington, D.C. 1963Description: 34.DDC classification: NASA | TN D-1959 -
| 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-1959 - (Browse shelf) | Not for loan | TR8715 |
Total holds: 0
Bound With Nasa Tn D-1951-1960
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