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ANGLE OF ATTACK ANALYSIS OF A SPINNING SLENDER CONE WITH SLIGHT AERODYNAMIC AND MASS ASYMMETRICS(REENTERY F)

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BookPublisher: Nasa, Washington, D.C. 1970Description: 35.DDC classification: NASA | TN D-5948

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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-5948 (Browse shelf)	Not for loan		TR15136

Total holds: 0

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Previous	NASA TN D-5944 WIND-TUNNEL INVESTIGATION OF VAROUS SMALL-SCALE RITIR/WING CONFIGURATIONS FOR VTOL COMPOSITE AIRCRAFT IN THE CRUISE MODE.	NASA TN D-5946 SI(N.P) AND SI (N.A) REACTION CROSS SECTIONS AT MEV NEUTRON ENERGY.	NASA TN D-5947 STRESS CONCENTRAIONS IN FILMENT-STRIFFENED SHEETS OF FINITE LENGTH.	NASA TN D-5948 ANGLE OF ATTACK ANALYSIS OF A SPINNING SLENDER CONE WITH SLIGHT AERODYNAMIC AND MASS ASYMMETRICS(REENTERY F)	NASA TN D-5949 NOMOLOGY OF EARTH-MOON ORBITS, C=4.00 AND C=C(LI)	NASA TN D-5951 APPROXIMATION FOR DISTRIBUTION OF FLOW PROPERTIES IN THE ANGLE-OF-ATTACK PLANE OF CONICAL FLOWS	NASA TN D-5952 A METHOD FOR PREDICTING PRESSURES ON ELLIPTIC CONES AT SUPERSONIC SPEEDS	Next

Bound With Nasa Tn D-5940-5947,5949.

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