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THE LONGITUDINAL RESPONSE OF A FLEXIBLE SLENDER AIRCRAFT TO RANDOM TURBULENCE

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BookPublisher: Her Majesty'S Stationery Office, London 1967Description: 43.DDC classification: ARC | R&M 3454

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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 3454 (Browse shelf)	Not for loan		TR14561

Total holds: 0

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Previous	ARC R&M 3420 FLIGHT MEASUREMENTS OF THE DRAG OF A SWEPT-WING AIRCRAFT(HUNTER MK.I) AT MACH NUMBERS UP TO 1.2,TOGETHER WITH SOME MEASUREMENTS OF LIFT-CURVE SLOPE	ARC R&M 3452 STUDIES OF SLOTTED-WALL INTERFERENCE USING AN ELECTRICAL ANALOGUE	ARC R&M 3453 THE CALCULATION OF GENERALISED FORCES ON OSCILLATING WINGS IN SUPERSONIC FLOW BY LIFTING SURFACE THEORY	ARC R&M 3454 THE LONGITUDINAL RESPONSE OF A FLEXIBLE SLENDER AIRCRAFT TO RANDOM TURBULENCE	ARC R&M 3455 WIND TUNNEL STUDIES OF LEADING EDGE SEPARATION PHENOMENA ON A QUARTER SCALE MODEL OF THE OUTER PANEL OF THE HANDLEY PAGE VICTOR' WING, WITH AND WITHOUT NOSE DROOP	ARC R&M 3456 THE UNSTEADY FORCES ON FINITE WINGS IN TRANSIENT MOTION	ARC R&M 3457 WIND TUNNEL TESTS OF A WING FITTED WITH A SINGLE LIFTING FAN	Next

Bound With Arc R&M 3451-3453,3455-3459

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