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FLIGHT VELOCITY EFFECTS ON JET NOISE OF SEVERAL VERIATIONS OF A TWELVE-CHUTE SUPPRESSOR INSTALLED ON A PLUG NOZZLE

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BookPublisher: Nasa, Washington, D.C. 1974Description: 36.DDC classification: NASA | TM X-2917 -

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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-2917 - (Browse shelf)	Not for loan		TR10355

Total holds: 0

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Previous	NASA TM X-288 AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4(DEGRE) TO 100(DEGRE) OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS	NASA TM X-289 FIN LOADS AND TIP-CONTROL HINGE MOMENTS ON A1/8-SCALE MODEL SIMULATING THE FIRST STAGE OF THE SCOUT RESEARCH VEHICLE AT A MACH NUMBER OF 2.01	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	Next

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