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FREE-FLIGHT SKIN-TEMPERATURE AND SURFACE-PRESSURE MEASUREMENTS ON A HIGHLY POLISHED NOSE HAVING A 100 (DEGRE) TOTAL -ANGLE CONE AND A 10 (DEGRE) HALF-ANGLE CONICAL FLARE SECTION UP TO A MACH NUMBER O

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BookPublisher: Nasa, Washington, D.C. 1961Description: 23.DDC classification: NASA | TN D-807

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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-807 (Browse shelf)	Not for loan		TR15841

Total holds: 0

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Previous	NASA TN D-804 INVESTIGATION AT HIGH SUBSONIC SPEEDS OF THE USE OF LOW AUXILIARY TAIL SURFACES HAVING DIHEDRAL TO IMPROVE THE LONGITUDINAL AND DIRECTIONAL STABILITY OF A T-TAIL MODEL AT HIGH LIFT	NASA TN D-805 TENSILE AND COMPRESSIVE CREEP OF 6A\|-4V TITANIUM-ALLOY SHEET AND METHODS FOR ESTIMATING THE MINIMUM CREEP RATE	NASA TN D-806 THE BEHAVIOR OF BERYLLIUM AND BERYLLIUM COPPER IN A 4,000(DEGRE) F SUPERSONIC AIR JET AT A MACH NUMBER OF 2	NASA TN D-807 FREE-FLIGHT SKIN-TEMPERATURE AND SURFACE-PRESSURE MEASUREMENTS ON A HIGHLY POLISHED NOSE HAVING A 100 (DEGRE) TOTAL -ANGLE CONE AND A 10 (DEGRE) HALF-ANGLE CONICAL FLARE SECTION UP TO A MACH NUMBER O	NASA TN D-808 AN EXPERIMENTAL INVESTIGATION OF THE DAMPING OF LIQUID OSCILLATIONS IN AN OBLATE SPHEROIDAL TANK WITH AND WITHOUT BAFFLES	NASA TN D-809 TABLES AND CHARTS OF THE NORMAL COMPONENT OF INDUCED VELOCITY IN THE LATERAL PLANE OF A ROTOR WITH HARMONIC AZIMUTHWISE VORTICITY DISTRIBUTION	NASA TN D-810 TOLERABLE LIMITS OF OSCILLATORY ACCELERATIONS DUE TO ROLLING MOTIONS EXPERIENCED BY ONE PILOT DURING AUTOMATIC-INTERCEPTOR FLIGHT TESTS	Next

Bound With Nasa Tn D-801-806,808-810

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