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To study the feasibility of developing the canopy of mushshaq aircraft without using mechanical fasteners G-67

By: Tashfeen; Prof Baber Saeed & Taimur Qureshi, advisorsPublisher: Risalpur NUST 2009Description: xii, 45 pDDC classification: PR 1414

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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 1414 (Browse shelf)	Available		CAEPR-1414

Total holds: 0

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Previous	PR 1410 study and analysis of the canopy shattering problem of K-8 aircraft	PR 1411 Installation of thrust measurement system on J-69 test bed	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	Next

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