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THE EFFECT OF CONICAL THICKNESS DISTRIBUTIONS ON THE SEPRATED FLOW PAST SLENDER DELTA WINGS.

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BookPublisher: Her Majesty'S Stationery Office, London 1971Description: 15.DDC classification: ARC | C.P 1189

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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 C.P 1189 (Browse shelf)	Not for loan		TR14462

Total holds: 0

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Previous	ARC C.P 1186 A FEASIBILITY STUDY ON A 200 VOLT, DIRECT CUURENT,AIRCRAFT ELECTRICAL POWER SYSTEM	ARC C.P 1187 EXPERIMENTAL INVESTIGATION OF A HIGH-LIFT LOW DRAG AEROFAIL.	ARC C.P 1188 CIVIL AIRCRAFT AIREOTHINESS DATA RECORDING PROGRAMME SPECIAL EVENTS OF METEROLOGICAL ORIGIN(JANUARY 1966 TO NOVEMBER 1968)	ARC C.P 1189 THE EFFECT OF CONICAL THICKNESS DISTRIBUTIONS ON THE SEPRATED FLOW PAST SLENDER DELTA WINGS.	ARC C.P 1190 AN EXPERIMENTAL INVESTIGATION OF SUPERSONIC BOUNDARY-LAYER FLOWS WITH PRESSURE GRADIENTS.	ARC C.P 472 FATIGUE LOADINGS IN FLIGHT - LOADS IN THE TAILPLANE OF A DEVON	ARC C.P 473 SOME INSTABILITIES ARISING FROM THE INTERACTIONS BETWEEN SHOCK WAVES AND BOUNDARY LAYERS	Next

Bound With Arc Cp-1181-1188,1190.

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