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LOW-SPEED WIND-TUNNEL INVESTIGATION OF BLOWING BOUNDARY-LAYER CONTROL ON LEADING-AND TRAILING-EDGE FLAPS OF A LARGE-SCALE, LOW-ASPECT-RATIO, 45(DEGREE)SWEPT-WING AIRPLANE CONFIGURATION

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BookPublisher: Nasa, Washington, D.C. 1959Description: 25.DDC classification: NASA | MEMO 1-23-59A -

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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 1-23-59A - (Browse shelf)	Not for loan		TR7777

Total holds: 0

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Previous	NASA MEMO 12-31-58L - FREE-FLIGHT HEAT-TRANSFER INVESTIGATION AT SUPERSONIC SPEEDS OF TWO SLENDER CONE-CYLINDER BODIES AT AN ANGLE OF ATTACK OF 8(DEGREE) WITH ONE BODY ROTATING	NASA MEMO 12-3-58L - ANALYSIS OF FLIGHT-TEST MEASUREMENTS OF THE WING STRUCTURAL DEFORMATIONS IN ROUGH AIR OF A LARGE FLEXIBLE SWEPT-WING AIRPLANE	NASA MEMO 12-3-58W HEAT TRANSFER IN THE TURBULENT INCOMPRESSIBLE BOUNDRY LAYER III- ARBITRARY WALL TEMPERATURE AND HEAT FLUX.	NASA MEMO 1-23-59A - LOW-SPEED WIND-TUNNEL INVESTIGATION OF BLOWING BOUNDARY-LAYER CONTROL ON LEADING-AND TRAILING-EDGE FLAPS OF A LARGE-SCALE, LOW-ASPECT-RATIO, 45(DEGREE)SWEPT-WING AIRPLANE CONFIGURATION	NASA MEMO 1-23-59L MAXIMUM MEAN LIFT COEFFICIENT CHARACTERISTICS AT LOW TIP MACH NUMBERS OF A HOVERING HELICOPTER ROTOR HAVING AN NACA 64 A012 AIRFOIL SECTION	NASA MEMO 12-4-58L - PRELIMINARY MEASUREMENT OF THE THE NOISE CHARACTERISTICS OF SOME JET-AUGMENTED CONFIGURATIONS	NASA MEMO 12-4-58W HEAT TRANSFER IN THE TURBULENT INCOMPRESSIBLE BOUNDRY LAYER IV- EFFECT OF LOCATION OF TRANSITION AND PREDICTION OF HEAT TRANSFER IN A KNOWN TRANSITION REGION.	Next

Bound With Nasa Memo 1-8-59a-1-29-59a

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