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AN EXPERIMENTAL INVESTIGATION OF THE CHARACTERISTICS OF AN OGEE WING FROM M=0.4 TO M=1.8

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BookPublisher: Her Majesty'S Stationery Office, London 1962DDC classification: C.P. | 585

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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	C.P. 585 (Browse shelf)	Not for loan Untraceable		TR10474

Total holds: 0

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Previous	C.P. 582 WIND TUNNEL TESTS AT MACH NUMBERS BETWEEN 0.6 AND 1.4 OF A 60 DEGREE SWEPT WING HAVING AN AEROFOIL SECTION DESIGNED FOR SUBCRITICAL FLOW AT A MACH NUMBER OF 1.2	C.P. 583 SURFACE OIL-FLOW PATTERNS ON WINGS OF DIFFERENT LEADING-EDGE RADIUS AND SWEEPBACK	C.P. 584 A SURVEY OF BUFFETING LOADS.	C.P. 585 AN EXPERIMENTAL INVESTIGATION OF THE CHARACTERISTICS OF AN OGEE WING FROM M=0.4 TO M=1.8	C.P. 586 THE ESTIMATION OF TRANSIENT TEMPERATURE DISTRIBUTIONS AND THERMAL STRESSES IN TURBINE AND COMPRESSOR DISCS.	C.P.1331 INTERFERENCE PROBLEMS ON WING-FUSELAGE COMBINATIONS	C.P.1334 INTERFERENCE PROBLEMS ON WING-FUSELAGE COMBINATIONS PART IV THE DESIGN PROBLEM FOR A LIFTING SWEPT WINNG ATTACHED TO A CYLINDRICAL FUSELAGE	Next

Bound With C.P.581-84 And 586-90

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