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The Structural Analysis of an Aircraft wing using Finite Element Method 41 "A" EC

By: Nabeel Zubair; Prof Javed Khan and Ejaz Mazhar (Advisors)Publisher: Karachi NED University 1994Description: 217pDDC classification: PR 1177

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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 1177 (Browse shelf)	Available		CAEPR-1177

Total holds: 0

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Previous	PR 1174 To study the thrust augumentation of Mirage A/C by water injection into the compressor inlet and comparison of results with the existing system	PR 1175 Experimental determination of bending/ totsional deflection of a thin metallic wing with a cutout and compaison with theoritical predictions using various types of finite elements	PR 1176 To Study the Effects of TIP Turbine or Vortex Turbine	PR 1177 The Structural Analysis of an Aircraft wing using Finite Element Method	PR 1178 Design and Fabrication of Hovercraft	PR 1179 Reduction of Aerodynamics Drag of Truck using Wind Tunnel	PR 118 Concealed object detection using fusion of visual and thermal images	Next

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