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LIFT,DRAG, AND PITCHING MOMENT OF AN ASPECT-RATIO-2 TRIANGULAR WING WITH LEADING-EDGE FLAPS DESIGNED TO SIMULATE CONICAL CAMBER

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BookPublisher: Nasa,Washington, D.C. 1958Description: 30.DDC classification: NASA | MEMO 10-5-58A

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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 10-5-58A (Browse shelf)	Not for loan		TR879

Total holds: 0

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Previous	NASA MEMO 10-26-58L FLIGHT INVESTIGATION OF A NORMAL-ACCELERATION AUTOMATIC LONGITUINAL CONTROL SYSTEM IN A FIGHTER AIRPLANE	NASA MEMO 10-27-58L HOVERING AND TRANSITION FLIGHT TESTS OF A 1/5-SCALE MODEL OF JET-POWERED VERTICAL-ATTITUDE VTOL RESEARCH AIRPLANE.	NASA MEMO 10-28-58L AERODYNAMIC CHRACTERISTICS OF SOME FAMILIES OF BLUNT BODIES AT TRANSONIC SPEEDS.	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	Next

Bound With Nasa Memo10-1-58a-1-4-58a,10-6-58a-10-8-58a.Lack No Nasa Memo-10-2-58a,10-7-58a.

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