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POWER-LAW VELOCITY-PROFILE-EXPONENT VARIATIONS WITH REYNOLDS NUMBER,WALL COOLING,AND MACH NUMBER IN A TURBULENT BOUNDARY LAYER.

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BookPublisher: Nasa, Washington, D.C. 1970Description: 57.DDC classification: NASA | TN D-5753

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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-5753 (Browse shelf)	Not for loan		TR14327

Total holds: 0

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Previous	NASA TN D-5729 AN EXPLORATORY WIND-TUNNEL INVESTIGATION OF THE WAKE EFFECT OF A PANEL TIP-MOUNTED FAN-JET ENGINE OF THE LIFT-INDUCED VORTEX	NASA TN D-5751 STUDY OF BRAYTON CYCLE POWER GENERATION SYSTEM USING SNAP-8 NUCLEAR REACTOR AS AN ENERGY SOURCE.	NASA TN D-5752 EXPERIMENTS ON THE STABILITY OF WATER-LUBRICATED THREE-SECTOR HYDRODYNAMIC JOURNAL BEARINGS AT ZERO LOAD.	NASA TN D-5753 POWER-LAW VELOCITY-PROFILE-EXPONENT VARIATIONS WITH REYNOLDS NUMBER,WALL COOLING,AND MACH NUMBER IN A TURBULENT BOUNDARY LAYER.	NASA TN D-5754 FLOW-FEED INVESTIGATION FOR LARGE-ANGLE CONES WITH SHORT SPIKES AT A MACH NUMBER OF 9.6	NASA TN D-5755 SONIC-BOOM CHRACTERISTICS IN THE EXTERME NEAR FIELS OF A COMPLEX AIRPLANE MODEL AT MACH NUMBERS OF 1.5,1.8 AND 2.5.	NASA TN D-5756 LEED AND AUGER STUDIES OF EFFECT OF OXYGEN ON ADHESION OF CLEAN IRON (001)AND (011) SURFACES.	Next

Bound With Nasa Tn D-5750-5752.5754-5759.

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