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TURBULENT BOUNDARY-LAYERS AND SKIN-FRICTION MEASUREMENTS IN AXIAL FLOW ALONG CYLINDERS AT MACH NUMBERS BETWEEN 0.5 AND 3.6.

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BookPublisher: Naca,Washington 1954Description: 53.DDC classification: NACA | TN-3097

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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	NACA TN-3097 (Browse shelf)	Not for loan		TR12136

Total holds: 0

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Previous	NACA TN-3094 THE RESISTANCE TO AIR FLOW OF POROUS MATERIALS SUITABLE FOR BOUNDARY-LAYER-CONTROL APPLICATIONS USING AREA SUCTION.	NACA TN-3095 THE AMES 10-BY 14-INCH SUPRESONIC WIND TUNNEL.	NACA TN-3096 THEORITICAL PREDICATION OF PRESSURE DISTRIBUTIONS ON NONLIFTING AIRFOILS AT HIGH SUBSONIC SPEEDS.	NACA TN-3097 TURBULENT BOUNDARY-LAYERS AND SKIN-FRICTION MEASUREMENTS IN AXIAL FLOW ALONG CYLINDERS AT MACH NUMBERS BETWEEN 0.5 AND 3.6.	NACA TN-3098 DENSITY PROFILES OF SUBSONIC BOUNDARY LAYERS ON A FLAT PLATE DETERMINED BY X-RAY AND PRESSURE MEASUREMENTS.	NACA TN-3099 IMPINGMENT OF WATER DROPLETS ON AN ELLIPSOID ITH FINESS RATIO 5 IN AXISMMETRIC FLOW.	NAL TN-SA-5-64/1964 A study of simply supported square plates with cutouts by the moire method and by finite differences	Next

Bound With Naca Tn-3090-96,3098-99.

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