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INITIAL LIFT OF FINITE ASPECT-RATIO WINGS DUE TO A SUDDEN CHANGE OF INCIDENCE

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BookPublisher: Her Majesty'S Stationery Office, London 1957Description: 6.DDC classification: ARC | R&M 3023

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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 3023 (Browse shelf)	Not for loan Untraceable		TR11121

Total holds: 0

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Previous	ARC R&M 3018 WIND-TUNNEL TESTS ON SEAPLANE HULLS IN THE R.A.E. 5-FT DIAMETER OPEN JET TUNNEL AND THE N.P.L. COMPRESSED AIR TUNNEL.	ARC R&M 3019 AN APPROXIMATE METHOD OF ESTIMATING THE EFFECT OF ELASTIC DEFORMABILITY OF THE AIRCRAFT STRUCTURE ON THE MANOEUVRE POINT.	ARC R&M 3021 THE EFFECT OF THE GROUND ON A HELICOPTER ROTOR IN FORWARD FLIGHT.	ARC R&M 3023 INITIAL LIFT OF FINITE ASPECT-RATIO WINGS DUE TO A SUDDEN CHANGE OF INCIDENCE	ARC R&M 3024 MEASUREMENTS OF THE EFFECT OF WINDSCREEN SHAPES ON THE DRAG OF COCKPIT CANOPIES AT TRANSONIC AND LOW SUPERSONIC SPEEDS USING THE FREE-FLIGHT-MODEL TECHNIQUE.	ARC R&M 3025 FLIGHT EXPERIMENTS ON BOUNDARY-LAYER CONTROL FOR LOW DRAG.	ARC R&M 3027 AN INVESTIGATION OF THE VELOCITY DISTRIBUTION AROUND THE NOSE OF THE AEROFOIL WITH A FLAP.	Next

Bound With Arc R&M 3020-21,3024-39 Lack No.3022,26,28,30,31,34,37

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