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WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.50 TO 1.14 OF THE STATIC AERODYNAMIC CHARACTERISTICS OF A MODEL OF A PROJECT MERCURY CAPSULE

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BookPublisher: Nasa,Washington, D.C. 1960Description: 28.DDC classification: NASA | TM X-292

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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-292 (Browse shelf)	Not for loan		TR13677

Total holds: 0

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Previous	NASA TM X-291 WIND-TUNNEL INVESTIGATION OF STATIC AERODYNAMIC CHARACTERISTICS OF A1/9-SCALE MODEL OF A PROJECT MERCURY CAPSULE AT MACH NUMBERS FROM 1.60 TO 4.65	NASA TM X-2917 - FLIGHT VELOCITY EFFECTS ON JET NOISE OF SEVERAL VERIATIONS OF A TWELVE-CHUTE SUPPRESSOR INSTALLED ON A PLUG NOZZLE	NASA TM X-2919 - FLIGHT VELOCITY EFFECTS ON JET NOISE OF SEVERAL VARIATIONS OF A 48-TUBE SUPPRESSOR INSTALLED ON A PLUG NOZZLE	NASA TM X-292 WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.50 TO 1.14 OF THE STATIC AERODYNAMIC CHARACTERISTICS OF A MODEL OF A PROJECT MERCURY CAPSULE	NASA TM X-294 ANALYTICAL INVESTIGATION AND PREDICTION OF SPIN AND RECOVERY CHARACTERISTICS OF THE NORTH AMERICAN X-15 AIRPLANE	NASA TM X-2951 - THRUST PERFORMANCE OF ISOLATED PLUG NOZZLES WITH TWO TYPES OF 40-SPOKE NOISE SUPPRESSOR AT MACH NUMBERS FROM 0 TO 0.45	NASA TM X-2963 - COMPATIBILITY OF REFRACTORY MATERIALS FOR NUCLEAR REACTOR POISON CONTROL SYSTEMS	Next

Bound With Nasa Tm X-281-291,294-299,Lack No.282,84-87,90,93,95,96,98

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