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THE PROPERTIES OF A THIN CONICALLY CAMBERED WING ACCORDING TO SLENDER-BODY THEORY

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BookPublisher: Her Majesty'S Stationery Office, London 1960Description: 19.DDC classification: ARC | R&M 3135

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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 R&M 3135 (Browse shelf)	Not for loan		TR10761

Total holds: 0

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Previous	ARC R&M 3132 DRAG READUCTION OF THIN WINGS AT SUPERSONIC SPEEDS, BY THE USE OF CAMBER AND TWIST.	ARC R&M 3133 BOUNDARY-LAYER MEASUREMENTS ON 15-DEG AND 24.5-DEG CONES AT SMALL ANGLES OF INCIDENCE AT M=3.17 AND 3.82 AND ZERO HEAT TRANSFER.	ARC R&M 3134 SUBSONIC WIND-TUNNEL TESTS OF VARIOUS FORMS OF AIR INTAKE INSTALLED IN A FIGHTER-TYPE AIRCRAFT	ARC R&M 3135 THE PROPERTIES OF A THIN CONICALLY CAMBERED WING ACCORDING TO SLENDER-BODY THEORY	ARC R&M 3136 SECONDARY FLOW AND LOSSES IN A COMPRESSOR CASCADE	ARC R&M 3137 THE CALCULATION OF LIFE SLOPES,ALLOWING FOR BOUNDARY LAYER, WITH APPLICATIONS TO THE RAE 101AND 104 AEROFOILS.	ARC R&M 3138 SOME EXPLORATORY JET-FLAP TESTS ON A 60-DEG DELTA WING.	Next

Bound With Arc R&M 3100-34, 3136-40 Lack No 3101-31

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