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CHOKING EFFECTS AND SOME REYNOLDS NUMBER EFFECTS ON THE MACH NUMBER DISTRIBUTION ROUND A TWO-DIMENSIONAL AEROFOIL IN THE RAE 10-FT X 7-FT HIGH-SPEED TUNNEL

By: Clarke,D A.

Contributor(s): ,H Egamble.

Material type: materialTypeLabel

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BookPublisher: Her Majesty'S Stationery Office, London 1955DDC classification: ARC | R&M 2912

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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	ARC R&M 2912 (Browse shelf)	Not for loan		TR18272

Total holds: 0

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Previous	ARC R&M 2907 AN APPROXIMATION TO THE MODE OF LONGITUDINALLY DISTURBED MOTION OF AN AIRCRAFT IN LEVEL FLIGHT	ARC R&M 2910 MODEL TESTS ON THE ASYMMETRY OF AIRFLOW OCCURRING IN TWIN-INTAKE SYSTEMS AT SUBSONIC SPEEDS	ARC R&M 2911 WIND-TUNNEL TESTS ON THE SYMMETRIC AND ANTISYMMETRIC FLUTTER OF SWEPT-BACK WINGS	ARC R&M 2912 CHOKING EFFECTS AND SOME REYNOLDS NUMBER EFFECTS ON THE MACH NUMBER DISTRIBUTION ROUND A TWO-DIMENSIONAL AEROFOIL IN THE RAE 10-FT X 7-FT HIGH-SPEED TUNNEL	ARC R&M 2913 TESTS ON A TYPICAL WHITTLE COMPRESSOR	ARC R&M 2915 THE DETERMINATION OF THE PRESSURE DISTRIBUTION OVER AN AEROFOIL SURFACE BY MEANS OF AN ELECTRICAL POTENTIAL ANALYSER	ARC R&M 2916 ABSTRACTS OF PAPERS PUBLISHED EXTERNALLY	Next

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