کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
292953 511091 2013 9 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Novel design and experimental validation of a contraction nozzle for aerodynamic measurements in a subsonic wind tunnel
موضوعات مرتبط
مهندسی و علوم پایه مهندسی انرژی انرژی های تجدید پذیر، توسعه پایدار و محیط زیست
پیش نمایش صفحه اول مقاله
Novel design and experimental validation of a contraction nozzle for aerodynamic measurements in a subsonic wind tunnel
چکیده انگلیسی


• A novel design for a contraction nozzle has been developed.
• Four different contractions were tested using the CFD package ANSYS FLUENT.
• Numerical results showed the benefits of the new profile.
• Experimental measurements have been conducted to characterize the performance of the new profile.
• Low levels of turbulence and high flow uniformity is confirmed at the nozzle discharge.

A novel design for a contraction nozzle, based on a logarithmic profile, is presented and developed to enhance aerodynamic measurements in a low-speed wind tunnel. The improvements obtained with this new proposal are validated, both, numerically and experimentally. As a starting point, four different wind tunnel contraction profiles were firstly considered and tested using the Computational Fluid Dynamics (CFD) package ANSYS FLUENT®. Both polynomial, due to its classical inclusion for wind tunnels, and logarithmic profiles, due to its expected enhancement, have been studied in terms of avoidance of separation of the boundary layer, procurement of a maximum level of exit-flow uniformity, and minimum turbulence levels at the outlet. Numerical comparison between obtained results shows the benefits of the new logarithmic profile developed by the authors, which was finally employed to construct the nozzle. To characterize its real performance, intensive experimental measurements have been conducted using pressure transducers and both single and dual hot wire anemometry. The pressure coefficient along the nozzle sidewall reveals an optimal evolution, matching perfectly with the theoretical design. In addition, low levels of turbulence and high flow uniformity is confirmed at the nozzle discharge. Turbulence intensities below 0.7% are obtained for the whole range of velocities available in the wind tunnel, and even practically constant uniform flow is obtained for all the traverses tested for validation. These indicators conclude that the contraction designed with the new profile is a good enhancing of the wind tunnel benefits.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Journal of Wind Engineering and Industrial Aerodynamics - Volume 118, July 2013, Pages 35–43
نویسندگان
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