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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..

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BookPublisher: Nasa, Washington, D.C. 1963Description: 34.DDC classification: NASA | TN D-1959 -

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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-1959 - (Browse shelf)	Not for loan		TR8715

Total holds: 0

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Previous	NASA TN D-1956 - AERODYNAMIC DAMPING OF A 0.02-SCALE SATURN SA-1 MODEL VIBRATING IN THE FIRST FREE-FREE BENDING MODE	NASA TN D-1957 - LOW SPEED INVESTIGATION OF THE EFFECTS OF WING SWEEP ON THE AERODYNAMIC CHARACTERISTICS OF PARAWINGS HAVING EQUAL-LENGTH LEADING EDGES AND KEEL	NASA TN D-1958 - TRANSONIC WIND-TUNNEL INVESTIGATION OF THE STATIC AERODYNAMIC CHARACTERISTICS OF SEVERAL CONFIGURATIONS OF THE BLUE SCOUT LAUNCH VEHICLE	NASA TN D-1959 - 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..	NASA TN D-1960 - SPAECTROMETRIC MEASUREMENTS OF GAS TEMPERATURES IN ARC-HEATED JETS AND TUNNELS	NASA TN D-1962 SUPERSONIC INVESTIGATION OF NOZZLE HINGE MOMENTS OF A MODIFIED STAURN C-1 MODEL WITH AND WITHOUT JET FLOW	NASA TN D-1977 A MICROMETOROID VELOCITY DETECTOR.	Next

Bound With Nasa Tn D-1951-1960

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