DESIGN, CONSTRUCTION AND TESTING OF LOW SPEED WIND TUNNEL WITH ITS MEASUREMENT AND INSPECTION DEVICES
محتوى المقالة الرئيسي
الملخص
A low speed open circuit wind tunnel has been designed, manufactured and constructed at the
Mechanical Engineering Department at Baghdad University - College of Engineering. The work is one of
the pioneer projects adapted by the R & D Office at the Iraqi MOHESR. The present paper describes the
first part of the work; that is the design calculations, simulation and construction. It will be followed by a
second part that describes testing and calibration of the tunnel. The proposed wind tunnel has a test
section with cross sectional area of (0.7 x 0.7 m2) and length of (1.5 m). The maximum speed is about (70
m/s) with empty test section. The contraction ratio is (8.16). Three screens are used to minimize flow
disturbances in the test section. The design philosophy is discussed and methods for wind tunnel
calculation are outlined. Simulation of wind tunnel using ANSYS shows no separation of flow along
wind tunnel. Construction steps are also included in present work.
تفاصيل المقالة
كيفية الاقتباس
تواريخ المنشور
المراجع
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R. Allan Wallis, ”Axial Flow Fan and Ducts”, John Wiley and sons, 1983.
Raikan S. Dawas, “Proposal for Subsonic Wind Tunnel Suitable in Iraq”, M.Sc.Thesis, University of Baghdad, September, 2001
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