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AN APPROXIMATE METHOD OF ESTIMATING THE EFFECT OF ELASTIC DEFORMABILITY OF THE AIRCRAFT STRUCTURE ON THE MANOEUVRE POINT.

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BookPublisher: Her Majesty'S Stationery Office, London 1957Description: 111.DDC classification: ARC | R&M 3019

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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 3019 (Browse shelf)	Not for loan		TR11052

Total holds: 0

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Previous	ARC R&M 3016 MEASUREMENTS OF THE PATHS OF THE VORTEX CORES SHED FROM THE WINGS OF A TYPICAL GUIDED-MISSILE MODEL AT M=I.57.	ARC R&M 3017 FLIGHT INVESTIGATION OF SOME AIRWORTHINESS PROBLEMS OF CIVIL BOAT SEAPLANES.	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.	Next

Bound With Arc R&M 3000-3018 Lack No. 3003,13,15.

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