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APPROACH AND LANDING INVESTIGATION AT LIFT-DRAG RATIOS OF 2 TO 4 UTILIZING A STRAIGHT-WING FIGHTER AIRPLANE

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BookPublisher: Nasa, Washington, D.C. 1960Description: 21.DDC classification: NASA | TM X-31 -

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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 TM X-31 - (Browse shelf)	Not for loan Untraceable		TR9331

Total holds: 0

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Previous	NASA TM X-3029 - CROSSFLOW EFFECTS ON IMPINGEMENT COOLING OF A TURBINE VANE	NASA TM X-3046 - MEASUREMENT OF GASEOUS EMISSIONS FROM A TURBOFAN ENGINE AT SIMULATED ALTITUDE CONDITIONS	NASA TM X-305 INVESTIGATION OF THE STATIC LONGITUDINAL STABILITY CHARACTERISTICS OF AN AIR-TO-SURFACE CANARD MISSILE CONFIGURATION IN THE TRANSONIC MACH NUMBER RANGE	NASA TM X-31 - APPROACH AND LANDING INVESTIGATION AT LIFT-DRAG RATIOS OF 2 TO 4 UTILIZING A STRAIGHT-WING FIGHTER AIRPLANE	NASA TM X-313 STRUCTURES FOR REENTRY HEATING	NASA TM X-314 EXPERIMENTAL STUDY OF A HOT STRUCTURE FOR A REENTRY VEHICLE	NASA TM X-317 WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.20 OF THE STATIC AERODYNAMIC AND CONTROL CHARACTERISTICS OF A MODEL OF A NONLIFTING REENTRY CAPSULE IN COMBINATION WITH A ROCKET BOOSTER	Next

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