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A DEVELOPED THEORY OF SPOILERS ON AEROFGOILS.

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BookPublisher: Her Majesty'S Stationery Office, London 1966Description: 44.DDC classification: ARC | C.P. 887

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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. 887 (Browse shelf)	Not for loan Untraceable		TR10577

Total holds: 0

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Previous	ARC C.P. 884 AN EXPERIMENTAL INVESTIGATION OF THE FLOW THROUGH INCLINED CIRCULAR TUBES AT A MACH NUMBER OF 4.0	ARC C.P. 885 A VELOCITY DEFECT RELATIONSHIP FOR THE OUTER PART OF EQUILIBRIUM AND NEAR EQUILIBRIUM TURBULENT BOUNDARY LAYERS.	ARC C.P. 886 PLASMA FLOW IN AN ELECTROMAGNETIC SHOCK TUBE AND IN A COMPRESSION SHOCK TUBE.	ARC C.P. 887 A DEVELOPED THEORY OF SPOILERS ON AEROFGOILS.	ARC C.P. 888 FORCE AND MOMENT MEASUREMENTS ON THREE DELTA WINGS OF ASPECT RATION 0.83, 1.03 AND 1.24 IN COMBINATION WITH BODIES OF FINENESS RATIO 13 AT A MACH NUMBER OF 4.	ARC C.P. 889 SOME EXPLORATORY TESTS ON A TWO-DIMENSIONAL BLOWN-CYLINDER MODEL IN THE R.A.E. 2FT.I1/2FT TRANSONIC WIND TUNNEL.	ARC C.P. 902 A PRELIMINARY FLIGHT SIMULATION STUDY OF JET -BORNE V.T.O.L. AIRCRAFT HANDLING QUALITIES	Next

Bound With Arc C.P.880-86 And 888-89

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