NUST Institutions Library Catalogue catalog › Details for: Determination of Velocity Profile for the improvement of Flow Quality of CAE 2x3 Subsonic Wind Tunnel. (2) To facilitate the Yawing motion of an aircraft model in the wind tunnel by fabricating and installing a rotating plateform and directional stability test of F-6 and F-7P AIRCRAFT MODELS

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Determination of Velocity Profile for the improvement of Flow Quality of CAE 2x3 Subsonic Wind Tunnel. (2) To facilitate the Yawing motion of an aircraft model in the wind tunnel by fabricating and installing a rotating plateform and directional stability test of F-6 and F-7P AIRCRAFT MODELS 44 "A" EC

By: Nauman Ahmed; Prof Shakeel (Advisor)Publisher: Karachi NED University 1996Description: 73pDDC classification: PR 1224

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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 1224 (Browse shelf)	Available		CAEPR-1224

Total holds: 0

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Previous	PR 1221 To Upgrade the existing Measurement System of the 2x3 CAE Subsonic Windtunnel by Incorporating the new Data Aquisition System	PR 1222 Aerodynamic Characteristics of a Wing in Incompessible Flow on the Basis of Thin Air foil Theory	PR 1223 Simulation of Aircraft Gas Turbine Engine	PR 1224 Determination of Velocity Profile for the improvement of Flow Quality of CAE 2x3 Subsonic Wind Tunnel. (2) To facilitate the Yawing motion of an aircraft model in the wind tunnel by fabricating and installing a rotating plateform and directional stability test of F-6 and F-7P AIRCRAFT MODELS	PR 1225 Code Developement in FORTRON	PR 1226 To Develop a Computer Code for Subsonic floe over the wings by using Singularity Distribution method	PR 1227 To write a computer code for the computation of take-off roll and monitoring the CG shift of a Mirage III aircraft	Next

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