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Preliminary design of a turbine for turbofan engine of a cruise missile

By: Aamir Abbas LashariPublisher: Risalpur NUST Risalpur 2001Description: 90p. Nisar AhmedDDC classification: PR 525

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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 525 (Browse shelf)	Available		CAEPR-525

Total holds: 0

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Previous	PR 522 Fabrication of solar water distillation plant	PR 523 Determination of loads spectrum of fatigue test panel specimen	PR 524 Effect of out of phase blowing and suction on a thick aerfoil	PR 525 Preliminary design of a turbine for turbofan engine of a cruise missile	PR 526 Designing and fabrication of laminated structures for impact resistance	PR 527 Normal Blowing and suction on a thin airfoil	PR 528 Design of 2-5 Ton gas absorption air conditioning unit	Next

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