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Preliminary design of the fan of a turbofan engine of a cruise missile

By: Muhammad Kamran SiddiquePublisher: Risalpur NUST Risalpur 2001Description: 60p. Khalid PervezDDC classification: PR 532

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Item type	Current location	Home library	Collection	Call number	Status	Date due	Barcode	Item holds
Book	College of Aeronautical Engineering (CAE)	College of Aeronautical Engineering (CAE)	NFIC	PR 532 (Browse shelf)	Available		CAEPR-532

Total holds: 0

Previous	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	Next
Previous	PR 53 Simulated Target shooter for firing range of Pakistan Air Force Academy Risalpur	PR 530 Modeling and structural analysis of super mushshak wing using ANSYS Software	PR 531 Development of a two node PC cluster for parallel processing using TCP/IP on a linux based operating system	PR 532 Preliminary design of the fan of a turbofan engine of a cruise missile	PR 533 Preliminary design of a compressor of turbofan engine for a cruise missile	PR 534 Computation of steady , inviscid, supersonic flow over an expansion corner	PR 535 Development of an artificial neural network to estimate the nozzle guide vane ext area of Atar 09C Engine	Next

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