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FLIGHT SIMULATOR INVESTIGATION OF THE EFFECT OF TURBULENCE ON ROLLING REQUIREMENTS AT LOW SPEED

By: Barnes,A.G.

Contributor(s): Parsons N.A.

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BookSeries: Aeronautical Research Council Reports And Memoranda R&M 3697. Publisher: DDC classification: R&M-3697

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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	R&M-3697 (Browse shelf)	Not for loan		TR6150

Total holds: 0

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Previous	R&M3620 MEASUREMENT OF THE MOMENTS AND PRODUCT OF INERTIA OF THE FAIREY DELTA 2 AIRCRAFT	R&M-3690 STUDY OF DYNAMIC AEROELASTIC EFFECTS ON THE STABILITY CONTROL AND GUST RESPONSE OF A SLENDER DELTA AIRCRAFT	R&m-3691 MEASUREMENT OR THE YAWING MOMENT OF INERTIA OF AN AIRCRAFT (HP 115) IN FLIGHTY	R&M-3697 FLIGHT SIMULATOR INVESTIGATION OF THE EFFECT OF TURBULENCE ON ROLLING REQUIREMENTS AT LOW SPEED	R&M-3707 COMPARISON OF WING PRESSURE DISTRIBUTIONS MEASUREDIN FLIGHT AND ON A WINDTUNNEL MODEL OF THE SUPER VC.10/BY G.C.BROWNE...[ET.AL]	R&M3708 REVIEW OF COMPARATIVE THEORETICAL AND EXPERIMENTAL AERODYNAMIC DATA RELEVANT TO ZERO- AND LOW- FREQUENCY AEROELASTIC PROBLEMS	R&M-3709 DISCRETE FREQUENCY SOUND GENERATION IN AXIAL FLOW TURBOMACHINES	Next

Bound With;Arc R&M3674-3697

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