Aerodynamical design of a low velocities wind tunnel

Authors

  • C. A. Quispe Gonzáles E. A. P. de Ingeniería Mecánica de Fluidos, Facultad de Ciencias Físicas, Universidad Nacional Mayor de San Marcos, Lima, Perú
  • W. J. Urcuhuaranga Esteban E. A. P. de Ingeniería Mecánica de Fluidos, Facultad de Ciencias Físicas, Universidad Nacional Mayor de San Marcos, Lima, Perú
  • J. E. Chiroque Baldera E. A. P. de Ingeniería Mecánica de Fluidos, Facultad de Ciencias Físicas, Universidad Nacional Mayor de San Marcos, Lima, Perú

DOI:

https://doi.org/10.15381/rif.v17i01.8664

Keywords:

Wind tunnel, aerodynamic analysis, tunnel admission, tunnel contraction, test section, difusor, tunnel fan.

Abstract

This paper aims to develop the aerodynamical design and the geometric detrmination of a low veñocities wind tunnel. Was elected an Eiffel type open wind tunnel, according to the required conditions in the test chamber, such as the area and maximum air velocity in the test section; we propose the constructive layout with the tunnel elements and the geometry of them. We performe calculations to determine the flow veloctiy, the cross section and the aerodynamical losses in the characteristic sections of the instalation. We determine the required fan power and it’s selection according to the local market conditions.

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Published

2014-07-15

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Article

How to Cite

Aerodynamical design of a low velocities wind tunnel. (2014). Revista De Investigación De Física, 17(01), 1-12. https://doi.org/10.15381/rif.v17i01.8664