Aerodynamic Coefficients Influence On The Performance Of Essay

PAGES
3
WORDS
1331
Cite

Aerodynamic Coefficients Influence on the Performance of LMR1 Car Car aerodynamics is governed by the same principles governing aircraft flights; the main focus being to produce down force instead of lift. In car aerodynamics, there is need to force more high speed-low pressure air to go under the car creating negative lift; down force (Rapid Racer, 2012). This results in higher grip levels for the tires and more traction, especially speeding around corners. For high performance cars, aerodynamics is achieved in several ways. The basic hypothesis is that faster driving increases down force thus pushing car's tires down resulting in higher grips and tractions during races. The downward force also known as drag is the square of the car's velocity; which is double the speed (Unlimited Performance Products, 2007). However, this increased down force reduces top speed resulting in more engine power to propel the car forward as shown below.

Nomenclature

In aerodynamics, there are several terms used unique to aerodynamics while some are used in unique ways when discussing aerodynamics. These include airfoil nomenclature, and glider axis among others.

The shape formed by the cross-section of a wing is known as airfoil and the round sides of the airfoil are leading edges (Rapid Racer, 2012). As the airfoil moves through the air, it experiences a relative wind and since the airfoil's gliders have forward and downward movements, the relative wind comes from the front and below the airfoil.

There are three axes of rotation intersecting at the glider's center of gravity with the glider's mass evenly distributed around the center of gravity. Movement about the pitch axis makes the glider's nose moves up or down while as it moves about the yaw axis, the nose moves from side to side. Additionally, whenever the glider rotates about the roll axis, one wing moves up, the other down.

Racing Car Aerodynamic

Drag is the force acting opposite to the path of the vehicle's motion. This force results in increased fuel consumption as it hinders vehicles top speed. According to manufacturers, low...

...

From this, FD is the drag force, ? is the air density, while V is the free stream velocity, and AF is the frontal area of the vehicle.
Lift is the force acting on vehicles as they move and may be manipulated to enhance the performance of a race car and decrease lap times as opposed to drag (Buresti, 2004). However, by manipulating the race car geometry it is possible to create negative lift, known as down force. Down force enhances vehicle performance by increasing the normal load on the tires. This increases the potential cornering force which results in the ability of the vehicle to corner faster and reduce lap times.

The lift of the vehicle is characterized by the lift coefficient (CL) and is calculated as; CL = FL / (1/2• •V2•AT) (2). In this equation, FL is the lift force; AT is the area of the top surface of the vehicle and the other. A negative lift coefficient shows a vehicle is experiencing down force.

Evaluation of Aerodynamic Forces

In aerodynamics, there are measures used to determine aerodynamic forces. The most common method is wind tunnels (Filip & Galetuse, 2011). This method is used in testing models of proposed aircraft and engine components. In this test, the model is situated in the test section of the tunnel and air made to flow past the model (National Aeronautics and Space Administration, 2012). Wind measurement encompasses four tests including measurement of aerodynamic forces directly, instrumenting the model with pressure taps and then calculating component performance from the pressure data (Society of Automotive Engineers, 2009). The other method is instrumenting the model to give diagnostic information regarding air flow around the model. The final method is using flow visualization techniques to provide diagnostic information.

Air velocity…

Sources Used in Documents:

References

Buresti, G. (2004). The Influence of Aerodynamics on the Design of High-Performance Road Vehicles. University of Pisa.

Filip, A., & Galetuse, S. (2011). Study of the Aerodynamic Forces Evaluation Methods. Incas Bulletin, 35-43.

Gal-Or, B. (1990). Vectored Propulsion, Supermaneuverability & Robot Aircraft. Springer Verlag.

Goldstein, E. (2010). Wind Tunnels, Don't Count Them Out. Aerospace America, Vol. 48 N0. 4, 38-43.
National Aeronautics and Space Administration. (2012, September 13). Wind Tunnel Testing. Retrieved October 25, 2012, from www.nasa.gov: http://www.grc.nasa.gov/WWW/k-12/airplane/tuntest.html
Rapid Racer. (2012). Aerodynamics. Retrieved October 25, 2012, from www.rapid-racer.com: http://www.rapid-racer.com/aerodynamics.php
The University of New South Wales. (2010). ACME Racing Design Report 2010. Retrieved October 25, 2012, from www.unsw.edu.au: http://seit.unsw.adfa.edu.au/studentactivities/saevehicle/car.php
Unlimited Performance Products. (2007). Aerodynamics. Retrieved October 25, 2012, from www.up22.com: http://www.up22.com/Aerodynamics.htm


Cite this Document:

"Aerodynamic Coefficients Influence On The Performance Of" (2012, October 26) Retrieved April 19, 2024, from
https://www.paperdue.com/essay/aerodynamic-coefficients-influence-on-the-82773

"Aerodynamic Coefficients Influence On The Performance Of" 26 October 2012. Web.19 April. 2024. <
https://www.paperdue.com/essay/aerodynamic-coefficients-influence-on-the-82773>

"Aerodynamic Coefficients Influence On The Performance Of", 26 October 2012, Accessed.19 April. 2024,
https://www.paperdue.com/essay/aerodynamic-coefficients-influence-on-the-82773

Related Documents

Integrating Schooling Fish Movement Into the Tree Wind Power Generators Model Tree wind generator turbine Structural loads in wind generator rotor blades have improved significantly as industrial generators have increased in proportions. This most impacts the style involving the inboard area of the blades, exactly where solid airfoil cross-sections have been essential to assist these strenuous loads (figure 1). Present inboard blades style endures efficiency losses from contending structural as well as

Su, Luo & Yun 2010
PAGES 10 WORDS 3491

This therefore renders the bifurcation point instability null and void for the cable strayed as well as suspension bridges (Ren,1999). Cheng, Jiang, Xiao and Xiang (2001) pointed out that in theory, the analysis of the aerostatic stability of such kinds of bridges should be regarded as a limit point instability challenge. In their paper, which is based on the limit point instability concept; Cheng, Jiang, Xiao and Xiang (2001)