NUST Institutions Library Catalogue catalog › Details for: To Investigate the Effect of Reynolds number, Oscillation rate, Thickness Ratio and Pivot point position on Dynamic stall of an Oscillating Airfoil

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To Investigate the Effect of Reynolds number, Oscillation rate, Thickness Ratio and Pivot point position on Dynamic stall of an Oscillating Airfoil Hussein Raza Hamdani CAEG-53 (A)

By: Saifur Rehman BakaulPublisher: Risalpur NUST 2001Edition: 1stDescription: 98pDDC classification: PR-516

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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-516 (Browse shelf)	Available		CAEPR-516

Total holds: 0

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Previous	PR-513 Torsional Testing of single cell tapered Box Beam	PR-514 Development of computer code for solution of Quasi one-dimensional isentropic flow through convergent-divergent nozzle	PR-515 To Find out the effects of Pitch rate, Reynolds number and Thickness on the dynamic stall of a Pitching Airfoil	PR-516 To Investigate the Effect of Reynolds number, Oscillation rate, Thickness Ratio and Pivot point position on Dynamic stall of an Oscillating Airfoil	PR-517 Design and development of an ASP-Based dynamic and interactive web application for technical human resource and Industrial Infrastructure of Pakistan	PR-518 Structural Analysis of UHF Antenna of F-16 Aircraft using ANSYS Software	PR-519 To design and Develop a PC Based flight Simulator for super Mushshak Aircraft	Next

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