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TUNNEL -WALL EFFECT ON AN AEROFOIL AT SUBSONIC SPEEDS

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BookPublisher: Her Majesty'S Stationery Office, London 1957Description: 19.DDC classification: ARC | R&M 2851

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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 2851 (Browse shelf)	Not for loan Untraceable		TR17043

Total holds: 0

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Previous	ARC R&M 2847 SIMPLE EVALUATION OF THE THEORETICAL LIFT SLOPE AND AERODYNAMIC CENTRE OF SYMMETRICAL AEROFOILS	ARC R&M 2849 DETAILED OBSERVATIONS MADE AT HIGH INCIDENCES AND AT HIGH-SUBSONIC MACH NUMBERS ON GOLDSTEN 1442/1547 AEROFOIL	ARC R&M 2850 PUBLISHED REPORTS AND MEMORANDA OF THE AERONAUTICAL RESERACH COUNCIL	ARC R&M 2851 TUNNEL -WALL EFFECT ON AN AEROFOIL AT SUBSONIC SPEEDS	ARC R&M 2854 THE CRITICAL WHIRLING SPEEDS AND NATURAL VIBRATIONS OF A SHAFT CARRYING A SYMMETRICAL ROTOR	ARC R&M 2855 OSCILLATING WINGS IN COMPRESSIBLE SUBSONIC FLOW	ARC R&M 2863 TESTS AT HIGH SUBSONIC SPEEDS ON A 10 PER CENT THICK PRESSURE-PLOTTING AEROFOIL OF RAE 104 SECTION	Next

Bound With Arc R&M-2841-2850,2852-2855.Lack No-2845,2846,2848,2852,2853.

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