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AERODYNAMIC LOADS ON AN ISOLATED SHROUDED-PROPELLER CONFIGURATION FOR ANGLES OF ATTACK FROM- 10 (DEGREE) TO 110 (DEGREE)

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BookPublisher: Nasa, Washington, D.C. 1961Description: 29.DDC classification: NASA | TN D-995

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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 TN D-995 (Browse shelf)	Not for loan		TR15884

Total holds: 0

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Previous	NASA TN D-992 STUDY OF FLOW OVER OSCILLATING AIRFOIL MODELS AT A MACH NUMBER OF 7.0 IN HELIUM	NASA TN D-993 STATIC LONGITUDINAL STABILITY OF A ROCKET VEHICLE HAVING A REAR-FACING STEP AHEAD OF THE STABILIZING FINS	NASA TN D-994 AERODYNAMIC CHARACTERISTICS OF TOWED CONES USED AS DECELERATORS AT MACH NUMBERS FROM 1.57 TO 4.65	NASA TN D-995 AERODYNAMIC LOADS ON AN ISOLATED SHROUDED-PROPELLER CONFIGURATION FOR ANGLES OF ATTACK FROM- 10 (DEGREE) TO 110 (DEGREE)	NASA TN D-996 AN ANALYTICAL TREND STUDY OF PROPELLER WHIRL INSTABILITY	NASA TN D-997 IN-FLIGHT NOISE MEASUREMENTS FOR THREE PROJECT MERCURY VEHICLES	NASA TN D-998 MEASUREMENTS OF TOTAL EMITTANCE OF SEVERAL REFRACTORY OXIDES, CERMETS,AND CERAMICS FOR TEMPERATURES FROM 600(DEGREE) F TO 2,000 (DEGRE) F	Next

Bound With Nasa Tn D-991-994,996-1000

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