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USE OF SIMILARITY PARAMETERS FOR EXAMINATION OF GEOMETRY CHARACTERISTICS OF HIGH-EXPANSION-RATIO AXIAL-FLOW TURBINES

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BookPublisher: Nasa, Washington, D.C. 1967Description: 33.DDC classification: NASA | TN D-4248

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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-4248 (Browse shelf)	Not for loan Untraceable		TR14009

Total holds: 0

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Previous	NASA TN D-4245 FREE-FLIGHT AERODYNAMIC CHARACTERISTICS OF A SLENDER CONE BETWEEN MACH NUMBERS OF 7 AND 8	NASA TN D-4246 MIDCOURSE-GUIDANCE PROCEDURE WITH SINGLE POSITION FIX OBTAINED FROM ONBOARD OPTICAL MEASUREMENTS	NASA TN D-4247 CHARTS FOR EQUILIBRIUM ISENTROPIC EXPANSION OF AIR BEHIND SHOCKS UP TO 50 000 FEET PER SEOOND (15.24 KILOMETERS PER SECOND)	NASA TN D-4248 USE OF SIMILARITY PARAMETERS FOR EXAMINATION OF GEOMETRY CHARACTERISTICS OF HIGH-EXPANSION-RATIO AXIAL-FLOW TURBINES	NASA TN D-4249 PERFORMANCE TESTS OF A 1/2-MILLIPOUND (2.2 MN) AMMONIA RESISTOJET THRUSTOR SYSTEM	NASA TN D-4250 HYDROGEN-OXYGEN CHEMICAL REACTION KINETICS IN ROCKET ENGINE COMBUSTION	NASA TN D-4252 INVISCID HYPERSONIC FLOW OVER A BLUNT BODY WITH HIGH RATES OF MASS AND HEAT TRANSFER	Next

Bound With Nasa Tn D-4241-4247,4249-4250

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