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study of separation control of a thick airfoil by varying MEMS parameters MS Aero / CFD

By: Ajmal BaigPublisher: Risalpur NUST 2002Description: viii, 92 pDDC classification: PR 1419

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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 1419 (Browse shelf)	Available		CAEPR-1419

Total holds: 0

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Previous	PR 1413 finite element modeling of mirage aircraft using commercially available finite element software, ANSYS	PR 1414 To study the feasibility of developing the canopy of mushshaq aircraft without using mechanical fasteners	PR 1418 Development of a 3D single block Grid Generation package for complex configurations	PR 1419 study of separation control of a thick airfoil by varying MEMS parameters	PR 142 Finite Element modeling and analysis of JF-17 aircraft	PR 1420 Design and Optimization of special purpose beam	PR 1422 structural design and analysis of four seater super Mushshak aircraft	Next

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