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Preliminary Design of a Turbofan Engine for a Cruise Missile Khalid Pervaiz CAEG-52 (A)

By: Umer IlyasPublisher: Risalpur NUST 2000Edition: 1stDescription: 93pDDC classification: PR 475

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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 475 (Browse shelf)	Available		CAEPR-475

Total holds: 0

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Previous	PR 472 Designing a database to Establish vital Factors for Reliability and Servicibility of MFI-17 A/C Components	PR 473 Designing and Development of a database system for the Directorate of Vehicles AHQ Islamabad	PR 474 Grid Generation on NACA 00'T' AIr Foil using Algebraic Method of CFD and writing a Fortran Code	PR 475 Preliminary Design of a Turbofan Engine for a Cruise Missile	PR 476 Manufacturing of K-8 Model for wind Tunnel Testing	PR 477 Transient Heat Conductin through a Rod by using Different explicit schemes of "CFD"	PR 478 Manufacturing of K-8 Model for Wind Tunnel Testing	Next

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