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A FLIGHT SIMULATION STUDY OF THE HANDLING CHARCTERISTICS OF A SLENDER WING SUPERSONIC TRANSPORT AIRCRAFT AT LANDING APPROACH SPEEDS

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BookPublisher: Her Majesty'S Stationery Office, London 1970Description: 61.DDC classification: ARC | R&M 3616

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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 3616 (Browse shelf)	Not for loan		TR16952

Total holds: 0

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Previous	ARC R&M 3611 FLIGHT MEASUREMENTS OF GROUND EFFECT ON THE LIFT AND PITCHING MOMENT OF A LARGE TRANSPORT AIRCRAFT (COMET 3B) AND COMPARISON WITH TUNNEL AND OTHER DATA.	ARC R&M 3612 AN ANTHROPOMETRIC SURVEY OF 200 R.A.F AND R.N AIRCREW AND THE APPLICATION OF THE DATA TO GARMENT SIZE ROLLS	ARC R&M 3615 THE DESIGN OF A DIGITAL THREE-TERM CONTROLLER AS A TURBOJET ENGINE SPEED GOVERNOR USING DIGITAL SINULATION METHODS	ARC R&M 3616 A FLIGHT SIMULATION STUDY OF THE HANDLING CHARCTERISTICS OF A SLENDER WING SUPERSONIC TRANSPORT AIRCRAFT AT LANDING APPROACH SPEEDS	ARC R&M 3617 LOW-SPED WIND-TUNNEL MEASUREMENTS OF OSCILLATORY ROLLING DERIVATIVES ON A SHARP-EDGED SLENDER WING.EFFECTS OF FREQUENCY PARAMETER AND OF GROUND	ARC R&M 3618 A NEW SERIES OF LOW-DRAG AEROFOILS	ARC R&M 3619 ANALYSIS OF THE STATIC PRESSURE DISTRIBUTION ON A DELTA WING IN SUBSONIC FLOW.	Next

Bound With Arc R&M-3613-3615,3617-3619.Lack No-3614

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