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THE TEST PERFORMANCE OF HIGHLY LOADED TURBINE STAGES DESIGNED FO HIGH PRESSURE RATIO

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BookPublisher: Her Majesty'S Stationery Office, London 1959Description: 30.DDC classification: ARC- | R&M 3242

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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 3242 (Browse shelf)	Not for loan Untraceable		TR10482

Total holds: 0

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Previous	ARC.R & M NO.3412 TRANSONIC COMPRESSOR NOISE THE EFFECT OF INLET GUIDE VANE/ROTOR SPACING	ARC .R & M NO.3413 THE SUPERSONIC FLOW PAS A CIRCULAR CONE AT INCIDENCE	ARC.R & M NO.3415 OSCILLATORY AERODYNAMIC FORCES IN LINEARISED SUPERSONIC FLOW FOR ARBITRARY FREQUENCIES,PLANFORMS AND MACH NUMBERS	ARC- R&M 3242 THE TEST PERFORMANCE OF HIGHLY LOADED TURBINE STAGES DESIGNED FO HIGH PRESSURE RATIO	ARC- R&M 3244 PRESSURE DISTRIBUTION AND SURFACE FLOW ON 5% AND 9% THICK WINGS WITH CURVED TIP AND 60 DEG SWEEPBACK	ARC 3204 THE EFFCT OF INTERNAL CONTRACTION, INITIAL RATE OF SUBSONIC DIFFUSION, AND COWL AND CENTREBODY SHAPE ON THE PRESSURE RECOVERY OF A CONICAL-CENTERBODY INTAKE AT SUPERSONIC SPEEDS.	ARC-A&M 3250 PUBLISHED REPORTS AND MEMORANDA OF THE AERONAUTICAL RESEARCH COUNCIL	Next

Bound With: Arc-R&M 3243-3260.

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