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Stress and modal analysis of a two stage axial flow compressor of a small turbefan engine G-62

By: Noman Tayyab; Abdul Munem Khan advisorPublisher: Risalpur NUST 2007Description: v, 50 pDDC classification: PR389

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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	PR389 (Browse shelf)	Available		CAEPR-389

Total holds: 0

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Previous	PR 386 Design and fabrication of thermally efficient gas geyser	PR 387 Develop a software for production planning and control of mirage aircraft components overhaul	PR388 To develop the capability of using 6 KVA AC generation system on mirage III ( non-ROSE) aircraft, originally equipped with a 9 KVA AC generation system	PR389 Stress and modal analysis of a two stage axial flow compressor of a small turbefan engine	PR 39 Early Warning Radar Simulation	PR 390 Aerodynamic analysis of the DA-20 EW upgrade suite	PR 391 design and proof of concept of a weapon capable unmanned aerial vehicle (UAV)	Next

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