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CROSSFLOW EFFECTS ON IMPINGEMENT COOLING OF A TURBINE VANE

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BookPublisher: Nasa, Washington, D.C. 1974Description: 19.DDC classification: NASA | TM X-3029 -

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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-3029 - (Browse shelf)	Not for loan		TR7564

Total holds: 0

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Previous	NASA TM X-3010 - SUMMARY OF THE RECENT SHORT-HAUL SYSTEMS STUDIES	NASA TM X-3017 - EFFECT OF SCREEN-INDUCED TOTAL-PRESSURE DISTORTION ON AXIAL-FLOW COMPRESSOR STABILITY	NASA TM X-3025 - MODIFICATION OF A THREE-DIMENSIONAL SUPERSONIC NOZZLE ANALYSIS AND COMPARISON WITH EXPERIMENT DATA	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	Next

Bound With Nasa Tm X-3006-46

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