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BLADE VIBRATORY STRESSES IN A MULTI-STAGE AXIAL-FLOW COMPRESSOR

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BookPublisher: Her Majesty'S Stationery Office, London 1958Description: 21.DDC classification: ARC | R&M 3181

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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 3181 (Browse shelf)	Not for loan Untraceable		TR16574

Total holds: 0

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Previous	ARC R&M 3178 THE STABILITY OF ROTOR BLADE FLAPPING MOTION.	ARC R&M 3179 HEAT TRANSFER AND LAMINAR-BOUNDARY-LAYER SEPRATION IN STAEDY COMPRESSIBLE FLOW PAST A WALL WITH NON-UNIFORM TEMERATURE	ARC R&M 3180 OBSERVATOINS OF THE FLOW OVER A TWO-DIMENSIONAL 4 PERCENT THICK AEROFOIL AT TRANSONIC SPEEDS.	ARC R&M 3181 BLADE VIBRATORY STRESSES IN A MULTI-STAGE AXIAL-FLOW COMPRESSOR	ARC R&M 3182 VORTEX-LATTICE TREATMENT OF RECTANGULAR WINGS WITH OSCILLATING CONTROL SURFACES	ARC R&M 3183 THE DESIGN AND TESTING OF AN AXIAL-FLOW COMPRESSOR HAVING DIFFERENT BLADE PROFILE IN EACH STAGE.	ARC R&M 3184 THE EFFECT OF REYNOLDS NUMBER ON THE PERFORMANCE OF A SINGLE-STAGE COMPRESSOR.	Next

Bound With Arc R&M-3171-3180,3182-3200.

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