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Model Analysis of a wing using ANSYS and the effect of wing tip missile on this analysis

By: Zawar A Nawaz, 016018Publisher: Risalpur NUST Risalpur 2004Description: vi, 47p. Zubair Islam, ProfDDC classification: PR 342

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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 342 (Browse shelf)	Available		CAEPR-342

Total holds: 0

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Previous	PR 34 Design and development of a broadband log-periodic antenna for hoght power transmissions	PR 340 Study and design of hydrogen fuel cell	PR 341 Designing / Fabrication of a test bench, capable of undertaking calibration / testing of differential pressure Gauges	PR 342 Model Analysis of a wing using ANSYS and the effect of wing tip missile on this analysis	PR 343 Make a computer program for the heat loading of a room	PR 344 Room air conditioner using natural gas at domestic pressure as energy source	PR 345 Design and manufacture air cushion vehicle that can dry wet play fields	Next

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