NUST Institutions Library Catalogue catalog › Details for: Shape optimization of JF-17 wing airfoil by le and te devices for drag reduction in supersonic flight regime

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Shape optimization of JF-17 wing airfoil by le and te devices for drag reduction in supersonic flight regime G-61

By: Irshad Faisal, Jehanzeb Masood & Omer Amin Prof. AdvisorsPublisher: Risalpur NUST 2005Description: 68 pDDC classification: PR 359

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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 359 (Browse shelf)	Available		CAEPR-359

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 356 To develop a computer program for determination of creep life consumption of a HPT blade (from available temperature history)	PR 357 Force and flow at low reynolds number during hovering motion	PR 358 To determine the aerodynamic co-efficients of JF-17 standard-1 weapons	PR 359 Shape optimization of JF-17 wing airfoil by le and te devices for drag reduction in supersonic flight regime	PR 36 Real time visual target tracking system using graphical processing unit (GPU)	PR 360 To study the underlying principles of laser doppler velocity meter and use it to determin the flow velocity	PR 361 To model the sample input files for various types of engines and write a user manual for future reference 9 for an already developed computer code for engine performance)	Next

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