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THE FLAPPING BEHAVIOUR OF A HELICOPTER ROTOR AT HIGH TIP-SPEED RATIOS.

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BookPublisher: Her Majesty'S Stationery Office, London 1966Description: 18.DDC classification: ARC | C.P. 877

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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 C.P. 877 (Browse shelf)	Not for loan		TR11010

Total holds: 0

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Previous	ARC C.P. 874 ANALYSIS OF HINGE MOMENT DATA FOR RECTANGULAR AND NEAR RECTANGULAR TRAILING EDGE CONTROLS AT SUPERSONIC AND TRANSONIC SPEEDS.	ARC C.P. 875 A NOTE ON THE TURBULENT UNIFORM-PROPERTY HYDRODYNAMIC BOUNDARY LAYER ON A SMOOTH IMPERMEABLE WALL; COMPARISIONS OF THEORY WITH EXPERIMENT.	ARC C.P. 876 CHARACTERISTICS OF HIGH-SPEED WIND TUNNEL IN THE UNITED KINGDOM RELEVANT TO AEROELASTIC-MODEL TESTS.	ARC C.P. 877 THE FLAPPING BEHAVIOUR OF A HELICOPTER ROTOR AT HIGH TIP-SPEED RATIOS.	ARC C.P. 878 COMPARISION OF HELICOPTER AND AEROPLANE VERTICAL ACCELERATIONS IN TURBULENCE.	ARC C.P. 879 ON THE INTERACTION OF THE TRANSMITTED SHOCK WITH THE BOUNDARY LAYER IN A SHOCK TUBE USING ARGON AS A TEST GAS.	ARC C.P. 881 THE INTERACTION OF THE REFLECTED SHOCK WITH THE BOUNDARY LAYER IN A SHOCK TUBE AND ITS INFLUANCE ON THE DURATION OF HOT FLOW IN THE REFLECTED-SHOCK TUNNEL. PART-1	Next

Bound With Arc C.P.869-76, 878-79

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