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OBSERVATIONS OF THE FLOW PAST A TWO-DIMENSIONAL 4 PER CENT THICK BICONVEX AEROFOIL AT HIGH SUBSONIC SPEEDS

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BookPublisher: Her Majesty'S Stationery Office, London 1958Description: 17.DDC classification: ARC | R&M 3092

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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 3092 (Browse shelf)	Not for loan Untraceable		TR14501

Total holds: 0

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Previous	ARC R&M 3047 A NUMERICAL METHOD FOR CALCULATING THE STARTING AND PERTURBATION OF A TWO-DIMENSIONAL JET AT LOW REYNOLDS NUMBER	ARC R&M 3049 THEORY OF AEROFOILS ON WHICH OCCUR BUBBLES OF STATIONARY AIR	ARC R&M 3091 AN EXPERIMENTAL INVESTIGATION OF LEADING-EDGE FLOW SEPARATION FROM A 4 PER CENT THICK TWO-DIMENSIONAL BICONVEX AEROFOIL	ARC R&M 3092 OBSERVATIONS OF THE FLOW PAST A TWO-DIMENSIONAL 4 PER CENT THICK BICONVEX AEROFOIL AT HIGH SUBSONIC SPEEDS	ARC R&M 3096 AN ANALYSIS OF STEADY STRAIGHT FLIGHT WITH INCLINED THRUST	ARC R&M 3097 THE DEVELOPMENT OF A VARIABLE-MACH-NUMBER EFFUSER	ARC R&M 3098 THE SHAPE OF THE CENTRE PART OF A SWEPT-BACK WING WITH A REQUIRED LOAD DISTRIBUTION	Next

Bound With Arc R&M3090-91,3096-98 Lack No.3093-3095

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