Experimental Evaluation for The Feasibility of Test Chamber in The Open-Loop Wind Tunnel

Author:

Ismail Ismail1,John Johanis2,Pane Erlanda Augupta1,Maulana Rahman2,Rahman Reza Abdu1,Suwandi Agri1

Affiliation:

1. Department of Mechanical Engineering, Faculty of Engineering Universitas Pancasila Srengseng Sawah, Jagakarsa 12640, Dki Jakarta, Indonesia

2. Student of Mechanical Engineering, Faculty of Engineering Universitas Pancasila Srengseng Sawah, Jagakarsa 12640, Dki Jakarta, Indonesia

Abstract

The test chamber in an open-loop wind tunnel is a critical part for aerodynamic experiment. The study aims to assess the feasibility of the new design of test chamber for open–loop wind tunnel by studying the fluid characteristic and the average pressure in the test chamber. The study is done by a series experimental test for the test chamber. From experimental test, the downstream velocity in the test chamber is increased from 8.9 m/s to 12.72 m/s where the pressure gradient is ranging from 6.19 to 8.398 atm with the overall turbulence intensity for the test chamber is 0.749%. According to the results, the designed open-loop wind tunnel is acceptable to use for an aerodynamic test.

Publisher

World Scientific and Engineering Academy and Society (WSEAS)

Subject

General Physics and Astronomy

Reference26 articles.

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3. D. B. Clarke, P. A. Brandner, and G. J. Walker, “Experimental and Computational Investigation of Flow Around a 3-1 Prolate Spheroid,” WSEAS Trans. FLUID Mech., vol. 3, no. 3, pp. 207–217, 2008.

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5. T. Morel, “Comprehensive Design of Axisymmetric Wind Tunnel Contractions,” J. Fluids Eng., pp. 1–9, 1975.

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