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MEASUREMENTS OF SECONDARY LOSS IN A MODEL TURBINE WITH VARIABLE INLET BOUNDARY LAYER

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Material type: Text

TextSeries: Aeronautical Research Council Current Papers ; C.P.No.1335Publication details: DDC classification:

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	C.P.1335 (Browse shelf(Opens below))	Not for loan		TR3352

Total holds: 0

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Previous	C.P. 586 THE ESTIMATION OF TRANSIENT TEMPERATURE DISTRIBUTIONS AND THERMAL STRESSES IN TURBINE AND COMPRESSOR DISCS.	C.P.1331 INTERFERENCE PROBLEMS ON WING-FUSELAGE COMBINATIONS	C.P.1334 INTERFERENCE PROBLEMS ON WING-FUSELAGE COMBINATIONS PART IV THE DESIGN PROBLEM FOR A LIFTING SWEPT WINNG ATTACHED TO A CYLINDRICAL FUSELAGE	C.P.1335 MEASUREMENTS OF SECONDARY LOSS IN A MODEL TURBINE WITH VARIABLE INLET BOUNDARY LAYER	C.P.1337 DESIGN AND THEORETICAL ASSESSMENT OF EXPERIMENT GLIDE PATH AND FLARE SYSTEMS FOR A BAC 1-11 AIRCRAFT (INCLUDING DIRECT LIFT CONTROL	CA-01 National geographic	CE77-01 NOTE ONN THE CALCULLATION OF FOURIER AMPLITUDE TRANSFORMS	Next

Bound With:Arc Cp-1331-1340

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