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HEAT-TRANSFER AND FRICTION MEASURMENT WITH VARIABLE PROPERTIES FOR AIRLOW NORMAL TO FINNED AND UNFINNED TUBE BANKS

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BookPublisher: Nasa, Washington, D.C. 1958Description: 33.DDC classification: NASA | MEMO 10-9-58E -

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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 10-9-58E - (Browse shelf)	Not for loan		TR7944

Total holds: 0

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Previous	NASA MEMO 10-5-58A LIFT,DRAG, AND PITCHING MOMENT OF AN ASPECT-RATIO-2 TRIANGULAR WING WITH LEADING-EDGE FLAPS DESIGNED TO SIMULATE CONICAL CAMBER	NASA MEMO 10-5-58E - STRUCTURAL DESIGN AND PRELIMINARY EVALUTION OF ALIGHT WEIGHT,BRAZED,AIR-COOLED TURBINE ROTOR ASSEMBLY	NASA MEMO 10-8-58A AN INVESTIGATION OF THE DRAG CHARACTERISTICS OF A TAILLESS DELTA-WING AIRPLANE FLIGHT, INCLUDING COMPARISON WITH WIND-TUNNEL DATA	NASA MEMO 10-9-58E - HEAT-TRANSFER AND FRICTION MEASURMENT WITH VARIABLE PROPERTIES FOR AIRLOW NORMAL TO FINNED AND UNFINNED TUBE BANKS	NASA MEMO 1-10-59A - TWO-DIMENSIONAL, SUPERSONIC, LINEARIZED FLOW WITH HEAT ADDITION	NASA MEMO 1-10-59L - HYDROGEN PEROXIDE HOT-JET SIMULATOR FOR WIND-TUNNEL TESTS OF TURBOJET-EXIT MODELS	NASA MEMO 11-4-58L - FLIGHT INVESTIGATION OF THE STABILITY AND CONTROL CHARACTERISTICS OF A 1/4-SCALE MODEL OF A TILT WING VERTICAL-TAKE OFF-AND-LANDING AIRCRAFT	Next

Bound With Nasa Memo 10-1-58e 1,5,9

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