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THE PRESSURE DRAG OF AN AEROFOIL WITH SIX DIFFERENCE ROUND LEADING EDGES, AT TRANSONIC AND LOW SUPERSONIC SPEEDS :

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BookPublisher: HER MAJESTY'S STATIONERY OFFICE,LONDON 1967Description: ,7.Subject(s): ENVIRONMENTAL CHEMISTRY | BIOGEOCHEMICAL CYCLESDDC classification: ARC C.P 921

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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 921 (Browse shelf)	Not for loan		86765

Total holds: 0

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Previous	ARC C.P 671 INFLATABLE SERVO ACTUATORS	ARC C.P 672 WIND TUNNEL TESTS AT SUPERSONIC SPEEDS ON A MODEL OF THE FAIREY DELTA 2	ARC C.P 901 A SURVEY OF UNSTEADY HYPERSONIC FLOW PROBLEMS	ARC C.P 921 THE PRESSURE DRAG OF AN AEROFOIL WITH SIX DIFFERENCE ROUND LEADING EDGES, AT TRANSONIC AND LOW SUPERSONIC SPEEDS	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 961 THE VELOCITY FIELD NEAR NON-LIFTIMG DELTA WINFS ACCORDING TO SUPERSONIC LINEARIZED THEORY.	ARC C.P 962 THE EFFECT OF BLEED ON THE PRESSURE OF SEVERAL SHROUDED AND UNSHROUDED PROPELLING NOZZLES AT M=1.96.	Next

Bound with ARC C.P.922-30

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