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HOVERING AND TRANSITION FLIGHT TESTS OF A 1/5-SCALE MODEL OF JET-POWERED VERTICAL-ATTITUDE VTOL RESEARCH AIRPLANE.

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BookPublisher: Nasa, Washington, D.C. 1958Description: 30.DDC classification: NASA | MEMO 10-27-58L

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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 10-27-58L (Browse shelf)	Not for loan Untraceable		TR11153

Total holds: 0

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Previous	NASA MEMO 10-23-58L EFFECTS OF BODY SHAPE ON THE DRAG OF A 45DEGREE OFSWEPTBACK-WING-BODY CONFIGURATION AT MACH NUMBERS FROM 0.90 TO 1.43.	NASA MEMO 10-25-58L HEAT-TRANSFER MEASUREMENTS OF TWO WING-BODY COMBINATIONS AT *DEGREE ANGLE OF ATTACK FROM A FLIGHT TEST FOR MACH NUMBERS TO 4.86 AND REYNOLDS NUMBERS TO 19.2	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	Next

Bound With:Nasa Memo-10-18-58l-10-26-58l,10-28-58l.Lack No-Nasa Memo-10-21-58l,10-24-58l.

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