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Designing/Optimization of Torsional Free all Composite UAV Wing by Utilizing Inherent Bending/Torsional Coupling Properties of Composite Materials 79 'A' EC

By: M. Waqas, Prof Haris and Sohail Ahmed (Advisors)Publisher: Islamabad NUST 2015Description: x,57pDDC classification: PR 2582

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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 2582 (Browse shelf)	Available		CAEPR-2582

Total holds: 0

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Previous	PR 258 Design and fabrication of Quad-rotor hovering UAV	PR 2580 Radar Cross Section Evaluation of JF-17 Aircraft with and without External Stores	PR 2581 Structural Analysis of Mounting Shroud of C - 130 Aircraft	PR 2582 Designing/Optimization of Torsional Free all Composite UAV Wing by Utilizing Inherent Bending/Torsional Coupling Properties of Composite Materials	PR 2583 The Effect of Fiber Morphology on Tensile Strength Subjected to Ballistic Impact	PR 2585 Experimental Study of Fan Performance and Air Bench Apparatus	PR 2586 Modeling and Simulation of Graphene Nanocomposites and their Possible Application in Aerospace Industry	Next

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