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NON-AXISYMMETRIC END-WALL BOUNDARY LAYER THEORY FOR AXIAL COMPRESSOR ROWA

By: Railly,J. W.

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BookSeries: Aeronautical Research Council Current Papers No.1322. Publisher: Her Majestys Stationery Office, London 1975Description: 20.DDC classification: TR | CP-1322

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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	TR CP-1322 (Browse shelf)	Not for loan		TR3339

Total holds: 0

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Previous	TR CP-1299 FLIGHT SIMULATION OF A WESSEX HELICOPTER A VALIDATION EXERCISE	TR CP-1300 LIST OF CURRENT PAPERS	TR CP-1321 CHARACTERISTICS OF A FAMILY OF ROOFLAP AEROFOILS DESIGNED AT THEIR DRAG-RISE CONDITION IN VISCOUS, COMPRESSIBLE FLOW	TR CP-1322 NON-AXISYMMETRIC END-WALL BOUNDARY LAYER THEORY FOR AXIAL COMPRESSOR ROWA	TR CP-1323 DEVELOPMENTS IN THE LIFTING SURFACE THEORY TREATMENT OF SYMMETRIC PLANFORMS WITH A LEADING EDGE CRANK IN SUBSONIC FLOW	TR CP-1324 ASSESSMENT OF THE ACCURACY OF SUBSONIC LINEARIZED THEORY FOR THE DESIGN OF WARPED SLENDER WINGS	TR CP-1325 SYSTEMS OF COORDINATES SUITABLE FOR THE NUMERICAL CALCULATION OF THREE-DIMENTIONAL FLOW FIELDS	Next

Bound With: Arc Cp 1321-1330

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