Research Papers: Flows in Complex Systems

Experimental and Numerical Validation of a Wind Gust Facility

[+] Author and Article Information
Raffaele Volpe

e-mail: raffaele.volpe@u-bourgogne.fr

Arthur Da Silva, Luis Le Moyne

Laboratoire DRIVE,
Institut Supérieur de l'Automobile
et des Transports,
Université de Bourgogne,
49 rue Mademoiselle Bourgeois,
58000 Nevers, France

Valérie Ferrand

Institut Supérieur de l'Aéronautique
et de l'Espace (ISAE),
Université de Toulouse,
10 avenue Edouard Belin,
31400 Toulouse, France

1Corresponding author.

Manuscript received May 21, 2012; final manuscript received December 6, 2012; published online January 18, 2013. Assoc. Editor: Z. C. Zheng.

J. Fluids Eng 135(1), 011106 (Jan 18, 2013) (9 pages) Paper No: FE-12-1254; doi: 10.1115/1.4023194 History: Received May 21, 2012; Revised December 06, 2012

The study of a vehicle moving through a lateral wind gust has always been a difficult task due to the difficulties in granting the right similitude. The facility proposed by Ryan and Dominy has been one of the best options to carry it out. In this approach, a double wind tunnel is used to send a lateral moving gust on a stationary model. Using this idea as a starting point, the ISAE has built a dedicated test bench for lateral wind studies on transient conditions. Experimental work has been carried out by means of time-resolved PIV, aiming at studying the unsteady interpenetration of the two flows coming from each wind tunnel. Meanwhile, a 3D CFD model based on URANS was set up, faithfully reproducing the double wind tunnel. Both the experimental and numerical results are compared, and the evolution of the reproduced wind gust is discussed. Conclusions are finally determined about the validity of this kind of test bench for ground vehicle applications.

Copyright © 2013 by ASME
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Fig. 1

Wind gust generator by use of an auxiliary wind tunnel

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Fig. 2

CAD drawing of the ISAE testbench

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Fig. 3

Projected side view scheme of a channel of the shutter system: (a) closed shutter configuration, and (b) open shutter configuration

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Fig. 4

Opening/closing door sequence scheme

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Fig. 5

Velocity vectors imposed by the two wind tunnels: (a) vector composition, and (b) expected time evolution of the longitudinal and transverse component of velocity at a generic point of the measurement zone

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Fig. 6

Part of the geometry from Fig. 2 (enlarged side view) with the position of the measurement plane

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Fig. 7

Three dimensional CFD: geometry and boundary conditions

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Fig. 8

Shutter system CFD simplification: (a) shutter boundary conditions, (b) comparison between real and simplified shutters, and (c) an example of the use of shutter boundary conditions

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Fig. 9

Unsteady gust; profiles of nondimensional velocity components at five points. A comparison of the TR-PIV data with the CFD models results. (a)–(e) Profile at the homonymous point, and (f) chosen points and measuring field positions.

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Fig. 10

Scheme explaining the unsteady profile of longitudinal velocity u+ in the test section. The “X” marks the considered point. (a) Pure longitudinal flow, (b) gust arrival, (c) steady gust, and (d) gust passage.

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Fig. 11

Unsteady gust; TR-PIV measurements versus the Spalart–Allmaras CFD simulations of the yaw angle field. (a) t+ = 3.79, (b) t+ = 7.97, and (c) t+ = 13.5.

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Fig. 12

Unsteady gust; profiles of the yaw angle β at five points. A comparison of the TR-PIV data with the CFD models results. (a)–(e) Profile at the homonymous point, and (f) chosen points and measuring field positions.




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