A History of Car Aerodynamics
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Glossary Physics (I-Introduction)
1 Glossary Physics (I-introduction) - Efficiency: The percent of the work put into a machine that is converted into useful work output; = work done / energy used [-]. = eta In machines: The work output of any machine cannot exceed the work input (<=100%); in an ideal machine, where no energy is transformed into heat: work(input) = work(output), =100%. Energy: The property of a system that enables it to do work. Conservation o. E.: Energy cannot be created or destroyed; it may be transformed from one form into another, but the total amount of energy never changes. Equilibrium: The state of an object when not acted upon by a net force or net torque; an object in equilibrium may be at rest or moving at uniform velocity - not accelerating. Mechanical E.: The state of an object or system of objects for which any impressed forces cancels to zero and no acceleration occurs. Dynamic E.: Object is moving without experiencing acceleration. Static E.: Object is at rest.F Force: The influence that can cause an object to be accelerated or retarded; is always in the direction of the net force, hence a vector quantity; the four elementary forces are: Electromagnetic F.: Is an attraction or repulsion G, gravit. const.6.672E-11[Nm2/kg2] between electric charges: d, distance [m] 2 2 2 2 F = 1/(40) (q1q2/d ) [(CC/m )(Nm /C )] = [N] m,M, mass [kg] Gravitational F.: Is a mutual attraction between all masses: q, charge [As] [C] 2 2 2 2 F = GmM/d [Nm /kg kg 1/m ] = [N] 0, dielectric constant Strong F.: (nuclear force) Acts within the nuclei of atoms: 8.854E-12 [C2/Nm2] [F/m] 2 2 2 2 2 F = 1/(40) (e /d ) [(CC/m )(Nm /C )] = [N] , 3.14 [-] Weak F.: Manifests itself in special reactions among elementary e, 1.60210 E-19 [As] [C] particles, such as the reaction that occur in radioactive decay. -
Drag Force Calculation
DRAG FORCE CALCULATION “Drag is the component of force on a body acting parallel to the direction of relative motion.” [1] This can occur between two differing fluids or between a fluid and a solid. In this lab, the drag force will be explored between a fluid, air, and a solid shape. Drag force is a function of shape geometry, velocity of the moving fluid over a stationary shape, and the fluid properties density and viscosity. It can be calculated using the following equation, ퟏ 푭 = 흆푨푪 푽ퟐ 푫 ퟐ 푫 Equation 1: Drag force equation using total profile where ρ is density determined from Table A.9 or A.10 in your textbook A is the frontal area of the submerged object CD is the drag coefficient determined from Table 1 V is the free-stream velocity measured during the lab Table 1: Known drag coefficients for various shapes Body Status Shape CD Square Rod Sharp Corner 2.2 Circular Rod 0.3 Concave Face 1.2 Semicircular Rod Flat Face 1.7 The drag force of an object can also be calculated by applying the conservation of momentum equation for your stationary object. 휕 퐹⃗ = ∫ 푉⃗⃗ 휌푑∀ + ∫ 푉⃗⃗휌푉⃗⃗ ∙ 푑퐴⃗ 휕푡 퐶푉 퐶푆 Assuming steady flow, the equation reduces to 퐹⃗ = ∫ 푉⃗⃗휌푉⃗⃗ ∙ 푑퐴⃗ 퐶푆 The following frontal view of the duct is shown below. Integrating the velocity profile after the shape will allow calculation of drag force per unit span. Figure 1: Velocity profile after an inserted shape. Combining the previous equation with Figure 1, the following equation is obtained: 푊 퐷푓 = ∫ 휌푈푖(푈∞ − 푈푖)퐿푑푦 0 Simplifying the equation, you get: 20 퐷푓 = 휌퐿 ∑ 푈푖(푈∞ − 푈푖)훥푦 푖=1 Equation 2: Drag force equation using wake profile The pressure measurements can be converted into velocity using the Bernoulli’s equation as follows: 2Δ푃푖 푈푖 = √ 휌퐴푖푟 Be sure to remember that the manometers used are in W.C. -
Chapter 4: Immersed Body Flow [Pp
MECH 3492 Fluid Mechanics and Applications Univ. of Manitoba Fall Term, 2017 Chapter 4: Immersed Body Flow [pp. 445-459 (8e), or 374-386 (9e)] Dr. Bing-Chen Wang Dept. of Mechanical Engineering Univ. of Manitoba, Winnipeg, MB, R3T 5V6 When a viscous fluid flow passes a solid body (fully-immersed in the fluid), the body experiences a net force, F, which can be decomposed into two components: a drag force F , which is parallel to the flow direction, and • D a lift force F , which is perpendicular to the flow direction. • L The drag coefficient CD and lift coefficient CL are defined as follows: FD FL CD = 1 2 and CL = 1 2 , (112) 2 ρU A 2 ρU Ap respectively. Here, U is the free-stream velocity, A is the “wetted area” (total surface area in contact with fluid), and Ap is the “planform area” (maximum projected area of an object such as a wing). In the remainder of this section, we focus our attention on the drag forces. As discussed previously, there are two types of drag forces acting on a solid body immersed in a viscous flow: friction drag (also called “viscous drag”), due to the wall friction shear stress exerted on the • surface of a solid body; pressure drag (also called “form drag”), due to the difference in the pressure exerted on the front • and rear surfaces of a solid body. The friction drag and pressure drag on a finite immersed body are defined as FD,vis = τwdA and FD, pres = pdA , (113) ZA ZA Streamwise component respectively. -
Automotive Design Culture: Aesthetic Trends Originated in Technology
F2004U060 AUTOMOTIVE DESIGN CULTURE: AESTHETIC TRENDS ORIGINATED IN TECHNOLOGY Liamadis, George*, Tsinikas, Nikolaos Faculty of Technology, School of Architecture, Aristotle University of Thessaloniki, Greece KEYWORDS - Design, Styling, Trends, Technology, Society ABSTRACT – Ever since the Futurist’s Manifesto, first to see the inner beauty of speed and progress symbolized in the form of early automobile’s mechanical parts, automotive history has often experienced paradigms of technological breakthroughs grown popular to establish aesthetic trends. The car, this highly influential cultural icon of the last century, has often drawn its stylistic inspiration in the product’s technological nature, in the attempt to express visually human’s inherent need for more power, for “better and faster”. Great pipes on early racing cars (1910’s), recalling images of “snakes with explosive breath”, had soon given their place in a new formal language, an aesthetic refinement known as streamlining (1930’s). The expressive force of streamlining, made it synonymous with ‘design’, sculptural intensity and ‘vigorous motion’ even when standing still. It provided an effective visual metaphor for progress, which soon became a formal topos and established an aesthetic trend later extended to a whole series of industrial products, often alien to the idea of motion. Aircraft-referential tailfins on American cars of the 50’s, took automotive styling into the supersonic age, expressing the power of flight and the optimism of the post-war period. The 1973 oil crisis brought up an automotive culture, which shifted the goal from maximization of speed to the optimization of effectiveness. Within this context, streamlining has retained its significance, now justified in terms of ecology and environmental politics. -
Numerical Optimization and Wind-Tunnel Testing of Low
Numerical Optimization and WindTunnel Testing of Low ReynoldsNumber Airfoils y Th Lutz W Wurz and S Wagner University of Stuttgart D Stuttgart Germany Abstract A numerical optimization to ol has been applied to the design of low Reynolds number airfoils Re The aero dynamic mo del is based on the Eppler co de with ma jor extensions A new robust mo del for the calculation of short n transitional separation bubbles was implemented along with an e transition criterion and Drelas turbulent b oundarylayer pro cedure with a mo died shap efactor relation The metho d was coupled with a commercial hybrid optimizer and applied to p erform unconstrained high degree of freedom optimizations with ob jective to minimize the drag for a sp ecied lift range One resulting airfoil was tested in the Mo del WindTunnel MWT of the institute and compared to the classical RG airfoil In order to allow a realistic recalculation of exp eriments conducted in the MWT the limiting nfactor was evaluated for this facility A sp ecial airfoil featuring an extensive instability zone was designed for this purp ose The investigation was supplemented by detailed measurements of the turbulence level Toget more insight in design guidelines for very low Reynolds numb er airfoils the inuence of variations of the leadingedge geometry on the aero dynamic characteristics was studied exp erimentally at Re Intro duction For the Reynoldsnumber regime of aircraft wingsections Re sophisticated di rect and inverse metho ds for airfoil analysis and design are available -
Aerodynamik, Flugzeugbau Und Bootsbau
Karosseriekonzepte und Fahrzeuginterior KFI INSPIRATIONEN DURCH AERODYNAMIK, FLUGZEUGBAU UND BOOTSBAU Dipl.-Ing. Torsten Kanitz Lehrbeauftragter HAW Hamburg WS 2011-12 15.11.2011 © T. Kanitz 2011 KFI WS 2011/2012 Inspirationen durch Aerodynamik, Flugzeugbau, Bootsbau 1 „Ein fortschrittliches Auto muss auch fortschrittlich aussehen “ Inspirationen durch Raketenbau / Torpedos 1913, Alfa-Romeo Ricotti Eine Vereinigung von Torpedoform und Eiförmigkeit Formale Aspekte im Vordergrund Bildquelle: /1/ S.157 aus: ALLGEMEINE AUTOMOBIL-ZEITUNG Nr.36, 1919 Ein Bemühen, die damaligen Erkenntnisse aus aerodynamischen Versuchen für den Automobilbau 1899 anzuwenden. Camille Jenatzy Schütte-Lanz SL 20, 1917 „Der rote Teufel“ Zunächst: nur optisch im Jamais Contente (Elektroauto) Die 100 km/h Grenze überschritten Bildquelle: /1/ S.45 Geschwindigkeitsrennen waren an der Tagesordnung aus: LA LOCOMOTION AUTOMOBILE, 1899 © T. Kanitz 2011 KFI WS 2011/2012 Inspirationen durch Aerodynamik, Flugzeugbau, Bootsbau 2 Inspirationen durch 1906 Raketenbau / Torpedos Daytona Beach „Stanley Rocket “ mit Fred Marriott Geschwindigkeitsweltrekord für Automobile mit Dampfantrieb mit beachtlichen 205,5 km/h Ein Bemühen, die damaligen Erkenntnisse aus aerodynamischen Versuchen für den Automobilbau Elektrotechniker anzuwenden. bedient Schaltungen Zunächst: nur optisch 1902 W.C. Baker Elektromobilfabrik 7-12 PS Elektromotor Torpedoförmiges Fichtenholzgehäuse Bildquelle: /1/ S.63 aus: Zeitschr. d. Mitteleuropäischen Motorwagen-Vereins, 1902 © T. Kanitz 2011 KFI WS 2011/2012 Inspirationen -
History of the Automobile
HISTORY OF THE AUTOMOBILE Worked by: Lara Mateus nº17 10º2 Laura Correia nº18 10º2 Leg1: the first car. THE EARLY HISTORY The early history of the automobile can be divided into a number of eras, based on the prevalent means of propulsion. Later periods were defined by trends in exterior styling, size, and utility preferences. In 1769 the first steam powered auto-mobile capable of human transportation was built by Nicolas-Joseph Cugnot. In 1807, François Isaac de Rivaz designed the first car powered by an internal combustion engine fueled by hydrogen. In 1886 the first petrol or gasoline powered automobile the Benz Patent-Motorwagen was invented by Karl Benz.This is also considered to be the first "production" vehicle as Benz made several identical copies. FERDINAND VERBIEST Ferdinand Verbiest, a member of a Jesuit mission in China, built the first steam-powered vehicle around 1672 as a toy for the Chinese Emperor. It was of small enough scale that it could not carry a driver but it was, quite possibly the first working steam-powered vehicle. Leg2: Ferdinand Verbiest NICOLAS-JOSEPH CUGNOT Steam-powered self-propelled vehicles large enough to transport people and cargo were first devised in the late 18th century. Nicolas-Joseph Cugnot demonstrated his fardier à vapeur ("steam dray"), an experimental steam-driven artillery tractor, in 1770 and 1771. As Cugnot's design proved to be impractical, his invention was not developed in his native France. The center of innovation shifted to Great Britain. NICOLAS-JOSEPH CUGNOT By 1784, William Murdoch had built a working model of a steam carriage in Redruth. -
Comparison of Wind Tunnel Airfoil Performance Data with Wind Turbine Blade Data
SERI/TP-254·3799 UC Category: 261 DE90000343 Comparison of Wind Tunnel Airfoil Performance Data with Wind Turbine Blade Data C. P. Butterfield G. N. Scott W. Musial July 1990 presented at the 25th lntersociety Energy Conversion Engineering Conference (sponsored by American Institute of Aeronautics and Astronautics) Reno, Nevada 12-17 August 1990 Prepared under Task No. WE011 001 Solar Energy Research Institute A Division of Midwest Research Institute 1617 Cole Boulevard Golden, Colorado 80401-3393 Prepared for the U.S. Department of Energy Contract No. DE-AC02-83CH1 0093 NOTICE This report was prepared as an account of work sponsored by an agency of the United States government. Neither the United States government nor any agency thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, com pleteness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise does not necessarily con stitute or imply its endorsement, recommendation, or favoring by the United States government or any agency thereof. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States government or any agency thereof. Printed in the United States of America Available from: National Technical Information Service U.S. Department of Commerce 5285 Port Royal Road Springfield, VA 22161 Price: Microfiche A01 Printed Copy A02 Codes are used for pricing all publications. -
UNIT – 4 FORCES on IMMERSED BODIES Lecture-01
1 UNIT – 4 FORCES ON IMMERSED BODIES Lecture-01 Forces on immersed bodies When a body is immersed in a real fluid, which is flowing at a uniform velocity U, the fluid will exert a force on the body. The total force (FR) can be resolved in two components: 1. Drag (FD): Component of the total force in the direction of motion of fluid. 2. Lift (FL): Component of the total force in the perpendicular direction of the motion of fluid. It occurs only when the axis of the body is inclined to the direction of fluid flow. If the axis of the body is parallel to the fluid flow, lift force will be zero. Expression for Drag & Lift Forces acting on the small elemental area dA are: i. Pressure force acting perpendicular to the surface i.e. p dA ii. Shear force acting along the tangential direction to the surface i.e. τ0dA (a) Drag force (FD) : Drag force on elemental area = p dAcosθ + τ0 dAcos(90 – θ = p dAosθ + τ0dAsinθ Hence Total drag (or profile drag) is given by, Where �� = ∫ � cos � �� + ∫�0 sin � �� = pressure drag or form drag, and ∫ � cos � �� = shear drag or friction drag or skin drag (b) Lift0 force (F ) : ∫ � sin � ��L Lift force on the elemental area = − p dAsinθ + τ0 dA sin(90 – θ = − p dAsiθ + τ0dAcosθ Hence, total lift is given by http://www.rgpvonline.com �� = ∫�0 cos � �� − ∫ p sin � �� 2 The drag & lift for a body moving in a fluid of density at a uniform velocity U are calculated mathematically as 2 � And �� = � � � 2 � Where A = projected area of the body or�� largest= � project� � area of the immersed body. -
The Austro Modern. Designers and Industrialists in the Innovation Network Austria - Czechoslovakia - Germany 1900 to 1939
The Austro Modern. Designers and Industrialists in the Innovation Network Austria - Czechoslovakia - Germany 1900 to 1939 (Source: www.tatra-club.com) Lecture at the Association of German Engineers, Berlin, Working Group History of Technology on March 11, 2021 Working Paper in the History of Mobility No. 24/2021 Richard Vahrenkamp Logistic Consulting Berlin Email: [email protected] Web: www.vahrenkamp.org Status: 28 March 2021 Content 1 Abstract ............................................................................................................................................... 2 2 Introduction ........................................................................................................................................ 3 4 Aircraft development at Austro Moderne ......................................................................................... 9 5 The designer Hans Ledwinka at Tatra .............................................................................................. 15 6 The role of the streamline in Austro Moderne ................................................................................ 20 7 The contribution of Bata to Austro Modernism .............................................................................. 25 8 Appendix diagram of the Austro network ........................................................................................ 28 9 Sources and literature ...................................................................................................................... -
Aerodyn Theory Manual
January 2005 • NREL/TP-500-36881 AeroDyn Theory Manual P.J. Moriarty National Renewable Energy Laboratory Golden, Colorado A.C. Hansen Windward Engineering Salt Lake City, Utah National Renewable Energy Laboratory 1617 Cole Boulevard, Golden, Colorado 80401-3393 303-275-3000 • www.nrel.gov Operated for the U.S. Department of Energy Office of Energy Efficiency and Renewable Energy by Midwest Research Institute • Battelle Contract No. DE-AC36-99-GO10337 January 2005 • NREL/TP-500-36881 AeroDyn Theory Manual P.J. Moriarty National Renewable Energy Laboratory Golden, Colorado A.C. Hansen Windward Engineering Salt Lake City, Utah Prepared under Task No. WER4.3101 and WER5.3101 National Renewable Energy Laboratory 1617 Cole Boulevard, Golden, Colorado 80401-3393 303-275-3000 • www.nrel.gov Operated for the U.S. Department of Energy Office of Energy Efficiency and Renewable Energy by Midwest Research Institute • Battelle Contract No. DE-AC36-99-GO10337 NOTICE This report was prepared as an account of work sponsored by an agency of the United States government. Neither the United States government nor any agency thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States government or any agency thereof. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States government or any agency thereof. -
Upwind Sail Aerodynamics : a RANS Numerical Investigation Validated with Wind Tunnel Pressure Measurements I.M Viola, Patrick Bot, M
Upwind sail aerodynamics : A RANS numerical investigation validated with wind tunnel pressure measurements I.M Viola, Patrick Bot, M. Riotte To cite this version: I.M Viola, Patrick Bot, M. Riotte. Upwind sail aerodynamics : A RANS numerical investigation validated with wind tunnel pressure measurements. International Journal of Heat and Fluid Flow, Elsevier, 2012, 39, pp.90-101. 10.1016/j.ijheatfluidflow.2012.10.004. hal-01071323 HAL Id: hal-01071323 https://hal.archives-ouvertes.fr/hal-01071323 Submitted on 8 Oct 2014 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. I.M. Viola, P. Bot, M. Riotte Upwind Sail Aerodynamics: a RANS numerical investigation validated with wind tunnel pressure measurements International Journal of Heat and Fluid Flow 39 (2013) 90–101 http://dx.doi.org/10.1016/j.ijheatfluidflow.2012.10.004 Keywords: sail aerodynamics, CFD, RANS, yacht, laminar separation bubble, viscous drag. Abstract The aerodynamics of a sailing yacht with different sail trims are presented, derived from simulations performed using Computational Fluid Dynamics. A Reynolds-averaged Navier- Stokes approach was used to model sixteen sail trims first tested in a wind tunnel, where the pressure distributions on the sails were measured.