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SYSTEMS OF COORDINATES SUITABLE FOR THE NUMERICAL CALCULATION OF THREE-DIMENTIONAL FLOW FIELDS

By: Mangler,K. W.

Contributor(s): Murray,J. C.

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BookSeries: Aeronautical Research Council Current Papers No.1325. Publisher: Her Majestys Stationery Office, London 1975Description: 68.DDC classification: TR | CP-1325

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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-1325 (Browse shelf)	Not for loan		TR3342

Total holds: 0

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Previous	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	TR CP-1326 LOW-SPEED WIND TUNNEL TESTS OF A TWO DIMENSIONAL WING FITTED WITH TWO PLAIN DIFFERENTIALLY-DEFLECTED TRAILING-EDGE FLAPS	TR CP-1327 THEORY OF PRACTICAL RETRACTION OF IMPERFECTLY ELASTIC ROPES	TR CP-1328 MEASUREMENTS OF PRESSURE DISTRIBUTION ON A HALF-MODEL WING BODY COMBINATION OF 55 DEG. SWEEP OVER A WIDE RANGE OF REYNOLDS NUMBER	Next

Bound With: Arc Cp 1321-1330

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