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EXPERIMENTAL INVESTIGATION OF THE PRESSURE RISE REQUIRED FOR INCIPIENT SEPARATION OF TURBULENT BOUNDARY LAYERS IN TWO-DIMENSIONAL SUPERSONIC FLOW

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BookPublisher: Nasa, Washington, D.C. 1959Description: 48.DDC classification: NASA | MEMO 1-21-59A -

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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 MEMO 1-21-59A - (Browse shelf)	Not for loan		TR7775

Total holds: 0

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Previous	NASA MEMO 12-13-58L - Transonic wind-tunnel investigation of the performance and of the static stability and control characteristics of a fighter- type airplane which embodies partial body indentation	NASA MEMO 12-14-58W STRUCTURE OF WEAK SHOCK WAVES IN A MONATOMIC GAS.	NASA MEMO 12-15-58L - FREE-FLIGHT INVESTIGATION OF A ROCKET-PROPELLED MODEL TO DETERMINE THE AERODYNAMIC HEATING ON A THIN, UNSWEPT, UNTAPERED, MULTISPAR, ALUMINUM -ALLOY WING AT MACH NUMBERS UP TO 2.22	NASA MEMO 1-21-59A - EXPERIMENTAL INVESTIGATION OF THE PRESSURE RISE REQUIRED FOR INCIPIENT SEPARATION OF TURBULENT BOUNDARY LAYERS IN TWO-DIMENSIONAL SUPERSONIC FLOW	NASA MEMO 12-20-58L - INVESTIGATION OF THE MAXIMUM SPIN-UP COEFFICIENT OF FRICTION OBTAINED DURING TESTS OF A LANDING GEAR HAVING A STATIC-LOAD RATING OF 20,000 POUNDS	NASA MEMO 12-21-58E EXPERIMENTAL INVESTIGATION OF COAXIAL JET MIXING OF TWO SUBSONIC STREAMS AT VARIOUS TEMPERATURE, MACH NUMBER, AND DIAMETER RATIOS FOR THREE CONFIGURATIONS	NASA MEMO 12-21-58L - TOTAL-PRESSURE RECOVERY AND DRAG CHARACTERISTICS OF SEVERAL AUXILIARY INLETS AT TRANSONIC SPEEDS	Next

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