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PRESSURE DISTRIBUTIONS ON BLUNT DELTA WINGS AT ANGLES OF ATTACK UP TO 90(DEGREE) AND MACH NUMBER OF 6.85

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BookPublisher: Nasa, Washington, D.C. 1963Description: 39.DDC classification: NASA | TN D-1954 -

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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-1954 - (Browse shelf)	Not for loan		TR8710

Total holds: 0

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Previous	NASA TN D-1940 - INVESTIGATION OF THE NATURAL FREQUENCIES AND MODE SHAPES OF DOUBLE CONICAL SANDWICH DISKS	NASA TN D-1952 - MEASURED VARIATION IN THE TRANSFER FUNCTION OF A HUMAN PILOT IN SINGLE-AXIS TASKS	NASA TN D-1953 - EVALUATION OF AN ELECTROMAGNETIC SHOCK TUBE FOR GENERATING STRONG SHOCK IN AIR	NASA TN D-1954 - PRESSURE DISTRIBUTIONS ON BLUNT DELTA WINGS AT ANGLES OF ATTACK UP TO 90(DEGREE) AND MACH NUMBER OF 6.85	NASA TN D-1955 - EFFECTS OF PEAK DECELERATION ON RANGE SENSITIVITY FOR A MODULATED-LIFT REENTRY AT SUPERCIRCULAR SPEEDS	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	Next

Bound With Nasa Tn D-1951-1960

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