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INDUCED PRESSURES AND SHOCK SHAPES ON BLUNT CONES IN HYPERSONIC FLOW

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BookPublisher: Nasa, Washington, D.C. 1964Description: 25.DDC classification: NASA | TN D-2182

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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-2182 (Browse shelf)	Not for loan		TR14840

Total holds: 0

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Previous	NASA TN D-2165 COMPRASION OF MEASUREMENTS OF INTERNAL TEMPERATURES IN ABLATION MATERIAL BY VARIOUS THERMOCOUPLE CONFIGURATIONS.	NASA TN D-217 LOW -SPEED INVESTIGATION OF STATIC LONGITUINAL AND LATERAL STABILITY CHRACTERISTICS OF AN AIRPLANE CONFIGURATION WITH A HIGHLY TAPERED WING AND WITH SEVRAL BODY AND TAIL ARRANGMENTS.	NASA TN D-218 LONGITUDINAL AERDYNAMIC CHRACTERISTICS OF A HIGH-SUBSONIC-SPEED TRASPORT AIRPLANE MODEL WITH A CAMBERED 40 DEGREE SWETBACK WING OF ASPECT RATIO 8 AT MACH NUMBERS TO 0.96.	NASA TN D-2182 INDUCED PRESSURES AND SHOCK SHAPES ON BLUNT CONES IN HYPERSONIC FLOW	NASA TN D-2183 PERFORMANCE CHARACTERISTICS OF A PREFORMED ELLIPTICAL PARACHUTE AT ALTITUDES BETWEEN 200,000 AND 100,000 FEET OBTAINED BY IN-FLIGHT PHOTOGRAPHY	NASA TN D-2184 FORCE-COEFFICIENT AND MOMENT-COEFFICIENT CORRELATIONS AND AIR-HELIUM SIMULATION FOR SPHERICALLY BLUNTED CONES	NASA TN D-2185 ABRIEF STUDY OF CLOSED-CIRCUIT TELEVISION FOR AIRCRAFT LANDING	Next

Bound With Nasa Tn D-2181,2183-2190

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