EFFECT OF NOSE BLUNTNESS,FINENESS RATIO,CONE ANGLE,AND MODEL BASE ON THE STATIC AERODYNAMIC CHARACTERISTICS OF BLUNT BODIES AT MACH NUMBER OF 1.57, 180,AND 2.16 AND ANGLE OF ATTACK UP TO 180 (DEGREE)
By: SHAW, DAVID S.
Contributor(s): Babb,C. Donald | FULLER,DENNIS E.
Material type:
BookSeries: NASA Technical Note. Publisher: NASA, WASHINGTON, D.C. 1967Description: 77p.Subject(s): AerodynamicsDDC classification: NASA | TN D-1781 -
| Item type | Current location | Collection | Call number | Vol info | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | NASA TN D-1781 | Not for loan | 101074 |
Total holds: 0
Technical Reports D-1781
Bound Vol. No.101074; TR8292-99
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