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
Publisher: Karachi NED University 1996Description: 73pDDC classification: PR 1224| Item type | Current location | Home library | Collection | Call number | Status | Date due | Barcode | Item holds |
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Book
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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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