HAN Automotive SEV Lesson 5: Aerodynamics Saving Energy in a Vehicle Note: most figures in this PowerPoint are from the reader SEV, others are directly sourced 1 content • • • • • • • • • 2 Static and dynamic pressure The relation between pressure and force Bernoulli’s Law Laminar and Turbulent Flows The influence of the border layer around objects Methods to lower the air resistance The drag force coefficient Calculate the power needed to overcome air resistance Stationary Mass Flow Static and Dynamic pressure Static Pressure πππππ£ = πβπ¦ππ = ο² β π β β Dynamic Pressure 1 2 πππ¦π = ο² π£ 2 [ππ] https://aviation.stackexchange.com/questions/36656/how-can-dynamic-and-static-pressure-be-explained?rq=1 3 Bernoulli’s Law ο²air=1.3 [kg/m3] Wind = 10 [m/s] 2 Wind Glass 1 3 Glass-plate = 2 [m2] Calculate the Force on the glass plate because of the wind 1 1 π1 + ο² π β1 + ο² π£12 = π2 + ο² π β2 + ο² π£22 2 2 1 1 105 + 1.3 β 9.81 β 0 + β 1.3 β 102 = π2 + 1.3 β 9.81 β 0 + β 1.3 β 02 2 2 π2 = 100 065 ππ This means for the Force on the glass plate: πΉ π = π΄ => πΉ = π β π΄ = 65 β 2 = 130 [π] 4 How high can we get the water ? Try to calculate the maximum height, while pumping with maximum vacuum. ο²water = 1000 [kg/m3] 2 Remember: π1 + ο² π β1 + 1 ο² 2 π£12 = π2 + ο² π β2 + 105 + 0 + 0 = 0 + 1000 β 9.81 β β2 + 0 β2 = 10.19 [π] 5 1 ο² 2 π£22 1 Venturi => the carburetor 1 2 1 2 π1 + ο² π β1 + ο² π£12 = π2 + ο² π β2 + ο² π£22 Who can prove with Bernoulli’s principle that the pressure in the venturi is lower? 6 1 1 π1 + π£12 = π2 + π£22 2 2 π1 + π ππππ = π2 + πππ π2 < π1 Aerodynamics in practice 7 Border layer (grenslaag [NL]) https://www.rideapart.com/articles/255508/when-motorcycle-helmets-look-like-golf-balls/ • • • • 8 the speed of the medium at the border layer of the object is always zero Polishing the surfaces of objects to lessen the drag forces is not always true Within the border layer the friction causes a drag force The dimples on the surface of a golf ball makes it easier for the air to leave the surface, the border layer becomes thinner and the friction is lower Pressure around the object 9 A few tips A few tips : • Avoid sharp edges at the front • when you need to use obstacles (like wipers…) make a dimple or edge in your construction to release the border layer. • Let the frontal area increase slowly at the front, but also at the rear! • Look at good practices on the internet. The drag force coefficient has the minimum value when you can reach the speed of sound. If not, then review the tips above 10 Drag force example A Mc Laren F1 has a power of 465 [kW] (around 630 [hp]), and has a top speed of 380 [km/h]. How much power is needed to overcome only the air resistance? We need some numbers of course: First we calculate the speed in [m/s] : ππ ο²πππ = 1.3 π3 ππ = 0.32 [−] π΄ = 1.8 [π2 ] 380 π£= = 105.5 [π/π ] 3.6 Now we fill in the formula for the Air resistance: πΉπππ 1 1 2 = ππ ∗ π΄ ∗ ο² π£ = 0.32 ∗ 1.8 ∗ ∗ 1.3 ∗ 105.52 = 4.17 [ππ] 2 2 The power is Force times velocity: π = πΉ ∗ π£ = 4.17 ∗ 105.5 = 440 [ππ] 11 stationary mass flow Definitions : παΆ ππ mass flow or mass flux with unit π παΆ volume flow or volume flux with unit π density with unit ππ π3 π΄ cross-sectional area with unit π2 For a cilindrical pipe 12 π΄= 1 2 ππ 4 π3 π stationary mass flow There is stationary flow if the mass which passes per unit of time remains constant. For a cilindrical pipe παΆ = π π΄ π£ = 1 2 πβπ 4 π π£ = constant In the case of a liquid the volume flow is also constant because a liquid is incompressible (density remains the same) παΆ = π π΄ π£ = π ππ παΆ = π΄ π£ = 13 1 2 π£ = constant πβπ 4 A liquid flows through a pipe that narrows παΆ 1 = παΆ 2 ⇒ π1 β π΄1 β π£1 = π2 β π΄2 β π£2 Because liquids are incompressible there follows π1 = π2 So π΄1 β π£1 = π΄2 β π£2 π£2 = 14 π1 2 π£1 π2 βΉ βΉ 1 ππ12 4 π£1 = π1 > π2 1 ππ22 4 βΉ π£2 βΉ π£2 > π£1 π12 π£1 = π22 π£2 A liquid flows through a pipe that narrows π£2 = π1 2 π£1 π2 twice as narrow βΉ four times faster three times narrower βΉ nine times faster four times narrower βΉ sixteen times faster 15 A liquid through a pipe that splits into two pipes παΆ 1 = παΆ 2 + παΆ 3 παΆ 1 = 16 ⇒ π β 14ππ2 β π£ 2 παΆ 1 = π β π΄ β π£ 2 π β 14ππ2 β π£ 3 + + πβπ΄βπ£ 3 Homework Aerodynamics Please study chapter 5 of the reader: Saving Energy in a Vehicle-Reader 2022.pdf: And do the exercises of week 5 see Education / Onderwijs Online 17