Showing posts with label wind tunnel. Show all posts
Showing posts with label wind tunnel. Show all posts

Tuesday, 10 October 2023

Aerodynamic Drag Reduction in a Passenger Vehicle Using Vortex Generator with Varying Yaw Angles: Detailed Study | Chapter 8 | Emerging Trends in Engineering Research and Technology Vol. 1

 Large money are aimed at minimizing capacity needed for force i.e., new downsized engines accompanying new aerodynamic devices for drag decline. For passenger cabs the aerodynamic drag force is the dominating opposition force at higher velocity. The car body is frequently optimized for reducing the drag fighting. Vortex generators belong to the type of boundary tier manipulators. Their function is to revitalize an adverse pressure gradient edge layer that is to say about to separate by transporting high push fluid from the outer part of the confine layer just before the low momentum district closer to the wall. In this exploratory investigation, the alternative of pressure coefficient, dynamic pressure, cooperative of lift and drag with and without whirlpool generators (VG) on the house of a utility vehicle have happened studied at varying swerve angles of VG. The yaw angles secondhand are 10°, 15° and 20°. To measure the effect of altering the vehicle frame, wind tunnel tests have been acted with 1:15 scaled model of the serviceableness vehicle with velocities of 2.42, 3.7, 5.42 and 7.14m/s. The experiments granted that a great improvement of the sleek drag force reduction maybe achieved with whirlpool generator.

Author(s) Details:

P. Gopal,
Department of Automobile Engineering, Anna University BIT Campus, Tiruchirappalli, Tamil Nadu, India.

T. Senthilkumar,
Department of Automobile Engineering, Anna University BIT Campus, Tiruchirappalli, Tamil Nadu, India.

Please see the link here: http://bp.bookpi.org/index.php/bpi/catalog/book/147

Thursday, 27 May 2021

Numerical and Experimental Investigation of Wind Load on Photovoltaic Panel Assemblies | Chapter 7 | Current Approaches in Science and Technology Research Vol. 4

 The aerodynamic research of solar panel assemblies and the determination of wind load are presented in this chapter. The task is solved in the first phase using a 1:1 computer simulation of the wind flow around the suggested rectangular assembly using the FLUENT ANSYS programme, followed by experimental measurements in the wind tunnel with a boundary layer (BLWT) in Bratislava. The solution's goal was to figure out the maximum pressure and suction wind loads on the top and bottom surfaces of panels. The greatest local pressure in each panel row as maximum values from all wind directions is represented by the resulting net pressure coefficient. The experimentally determined net pressure coefficient values were compared to computer simulations and processes described in STN EN 1991-1-4. It is clear that the inner panels are loaded far less than the norm requires. The panels on the side of the assembly or along the aisle's edge are loaded substantially higher than the norm allows. In addition, frontal panels are less wind-stressed than the norm specifies.

Author(s) Details

Ol'ga Hubová
Slovak University of Technology, 810 05 Bratislava, Slovakia.

Michal Franek
Slovak University of Technology, 810 05 Bratislava, Slovakia.

Marek Macák
Slovak University of Technology, 810 05 Bratislava, Slovakia.

View Book :- https://stm.bookpi.org/CASTR-V4/article/view/1041