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THE EFFECT OF BLEED ON THE PRESSURE OF SEVERAL SHROUDED AND UNSHROUDED PROPELLING NOZZLES AT M=1.96.

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BookPublisher: Her Majesty'S Stationery Office, London 1966Description: 24.DDC classification: ARC | C.P 962

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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 962 (Browse shelf)	Not for loan Untraceable		TR14432

Total holds: 0

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Previous	ARC C.P 629 AERODYNAMIC AND MECHANICAL TESTS OF A MODEL OF A VARIABLE MACH NUMBER NOZZLE.	ARC C.P 672 WIND TUNNEL TESTS AT SUPERSONIC SPEEDS ON A MODEL OF THE FAIREY DELTA 2	ARC C.P 922 INVESTIGATION OF THE NORMAL FORCE CHARACTERISTICS OF SLENDER DELTA WINGS WITH VARIOUS RHOMBIC CROSS-SECTIONS IN SUBSONIC CONICAL FLOW	ARC C.P 962 THE EFFECT OF BLEED ON THE PRESSURE OF SEVERAL SHROUDED AND UNSHROUDED PROPELLING NOZZLES AT M=1.96.	ARC C.P 963 THE CALCILATION OF MOMENTUM THICKNESS IN A TURBULENT BOUNDARY LAYER AT MACH NUMBERS UP TO UNITY.	ARC C.P 964 A PRELIMENTAL INVESTIGATION OF SHOCK-WAVE DEVELOPMENT ON AEROFOILES.	ARC C.P 965 HEAT YRANSFER IN THE VICINITY OF A 15 DEGREE COMPRESSION CORNER AT MACH NUBMERS FROM 2.5 TO 4.4.	Next

Bound With Arc C.P-961,963-970.

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