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THE CALCULATION OF THE PRESSURE DISTRIBUTION ON A THICK CAMBERED AEROFOIL AT SUBSONIC SPEEDS INCLUDING THE EFFECTS OF THE BOUNDARY LAYER.

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BookPublisher: Her Majesty'S Stationery Office, London 1967Description: 30.DDC classification: ARC | C.P. 1005

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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. 1005 (Browse shelf)	Not for loan		TR10830

Total holds: 0

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Previous	ARC C.P. 1002 THE DEVELOPMENT AT CRANFIELD OF A FREE PISTON COMPRESSION SHOCK TUBE.	ARC C.P. 1003 AIRCRAFT LOADING ACTIONS PROBLEMS - PROCEEDINGS OF A SYMPOSIUM HELD AT FARNBOROUGH ON 28TH OCT.1966.	ARC C.P. 1004 THE NEW SYSTEM FOR CONTROLLING THE ATTITUDE AND MOTIVATOR DEFLECTIONS OF A MODEL IN THE R.A.E. NO.19 WIND TUNNEL.	ARC C.P. 1005 THE CALCULATION OF THE PRESSURE DISTRIBUTION ON A THICK CAMBERED AEROFOIL AT SUBSONIC SPEEDS INCLUDING THE EFFECTS OF THE BOUNDARY LAYER.	ARC C.P. 1006 THE LONGITUDINAL CHARACTERISTICS OF THREE SLENDER MILD OGEE WINGS AT MACH NUMBERS FROM 0.4 TO 2.0	ARC C.P. 1007 LOW-SPEED MEASUREMENTS OF SKIN FRICTION ON A LARGE HALF-MODEL SLENDER WING.	ARC C.P. 1008 DIFFRACTION OF BLAST WAVES FOR THE OBLIQUE CASE.	Next

Bound With Arc C.P.1000-1004, 1006-1009

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