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FULL-SCALE WIND-TUNNEL INVESTIGATION OF A JET FLAP IN CONJUNCTION WITH A PLAIN FLAP WITH BLOWING BOUNDARY-LAYER CONTROL ON A 35(DEGREE) SWEPTBACK-WING AIRPLANE

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BookPublisher: Nasa, Washington, D.C. 1959Description: 35.DDC classification: NASA | MEMO 2-20-59A -

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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 2-20-59A - (Browse shelf)	Not for loan		TR7523

Total holds: 0

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Previous	NASA MEMO 2-18-59W - THE INTERACTION OF AN OBLIQUE SHOCK WAVE WITH ALAMINAR BOUNDARY LAYER	NASA MEMO 2-19-59A - EXPERIMENTAL INVESTIGATION OF CIRCULAR INTERNAL-COMPRESSION INLETS WITH TRANSLATING CENTERBODIES EMPLOYING BOUNDARY-LAYER REMOVAL AT MACH NUMBERS FROM 0.85 TO 3.50	NASA MEMO 2-19-59L - FLIGHT INVESTIGATION OF AN AUTOMATIC THROTTLE CONTROL IN LANDING APPROACHES	NASA MEMO 2-20-59A - FULL-SCALE WIND-TUNNEL INVESTIGATION OF A JET FLAP IN CONJUNCTION WITH A PLAIN FLAP WITH BLOWING BOUNDARY-LAYER CONTROL ON A 35(DEGREE) SWEPTBACK-WING AIRPLANE	NASA MEMO 2-20-59E A 20,000-KILOWATT NUCLEAR TURBOELECTRIC POWER SUPPLY FOR MANNED SPACE VEHICLES	NASA MEMO 2-20-59L - TABLES FOR THE RAPID ESTIMATION OF DOWNWASH AND SIDEWASH BEHIND WINGS PERFORMING VARIOUS MOTIONS OF SUPERSONIC SPEEDS	NASA MEMO 2-21-59L - STUDY OF TAXIING PROBLEMS ASSOCIATED WITH RUNWAY ROUGHNESS	Next

Bound With Nasa Memo 2-3-59a-2-27-59a

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