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TABLES FOR THE RAPID ESTIMATION OF DOWNWASH AND SIDEWASH BEHIND WINGS PERFORMING VARIOUS MOTIONS OF SUPERSONIC SPEEDS

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BookPublisher: Nasa, Washington, D.C. 1959Description: 177.DDC classification: NASA | MEMO 2-20-59L -

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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 2-20-59L - (Browse shelf)	Not for loan		TR7541

Total holds: 0

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Previous	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	NASA MEMO 2-22-59L - SOME STATIC, OSCILLATORY, AND FREE-BODY TESTS OF BLUNT BODIES AT LOW SUBSONIC SPEEDS	NASA MEMO 2-23-59L - TIRE-TO-SURFACE FRICTION ESPECIALLY UNDER WET CONDITIONS	Next

Bound With Nasa Memo 2-15-59l-2-28-59l

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