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A FEASIBILITY STUDY ON A 200 VOLT, DIRECT CUURENT,AIRCRAFT ELECTRICAL POWER SYSTEM

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BookPublisher: Her Majesty'S Stationery Office, London 1971Description: 44.DDC classification: ARC | C.P 1186

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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 1186 (Browse shelf)	Not for loan Untraceable		TR14459

Total holds: 0

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Previous	ARC C.P 1183 VERTICAL COCKPIT ACCELERATIONS MEASURED ON AN OPERATIONAL JET TRANSPORT AIRCRAFT.	ARC C.P 1184 AN INVESTIGATION OF THE PRESSURE DISTRIBUTIONS ON A 45 DEGREE SWEPT HALF WING INCLUDING THE EFFECTS OF UPPER SURFACE SPOLIERS.	ARC C.P 1185 CUMUATIVE DAMAGE IN FATIGUE WITH PARICULAR REFERENCE TO THE EFFECTS OF RESIDUAL STRESSES	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.	Next

Bound With Arc Cp-1181-1185,1187-1190.

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