Design presentation Aerodynamics

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SRN: 19034635. Design presentation Aerodynamics. Yellow pool float on water.

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What is Aerodynamics?. A branch of dynamics specially interested in the motion of air when interacting with objects.

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What is an Airfoil?. It produces forces when in motion to surrounding air. Its main objective is to generate significant lift when in motion. Used as basic form of wing..

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Diagram Description automatically generated with medium confidence.

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What is Drag?. Mechanical force Aerodynamic force working against aircraft motion (Thrust) Generated through difference in velocity between solid objects & fluid..

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Person writing on a notepad. Project background Concepts Planning (Logbook, Gantt chart) Design Activities/ process Feedback & results.

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Background. Aim, design a wing that has good performance in many areas: minimum drag Pitching moment Stall behaviour.

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LIZÆ7LYVÜf'IJ. Concept: Existing solutions.

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ATR 72 wing air foil. Research:. A picture containing shoji, building Description automatically generated.

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Pens and rulers. Plan.

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Timeline Description automatically generated.

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A picture containing text Description automatically generated.

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Design Activities. Design a Short-haul turboprop Typically used as a regional airliner passenger. De Havilland Canada DHC-8. Design activity 1: Calculating Cruising speed, cruising Altitude and all up weight. Design Activity 2: Calculating, lift in level flight. Design Activity 3: Finding aspect ratio via graph, lift coefficient and ideal coefficient.

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Design Activity 3. 40 35 30 20 10 GA Gliders Mil. surveillance Airliners T ransports 3 co 400 600 F i g hters 700.

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Periodic table of elements. Calculate: Dynamic viscosity Reynolds Number Chord Length Mach Number Generate airfoil on XFLR5 and analyse graphs.

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Design Activity 4. Thinness (8) at at Points TE nap TE xmnge Center I ine C : 'Users, style 9.04 29.40 0.00 0.00 0.00 0.00 o. 00 Ltay Sazgin/tesktcp/aizfo— 14.S3 25.43 0.00 0.00 0.00 12. SO 0.00 0.00 0.00 in the client area.

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Design Activity 4. o.m5 SargLn/Desktop/aIzZoii.dat Re€iO.ooo no.oo N9.o Tl Re610.OOO go.oo N9.O Re€10.ooo HO.4S N9.O 0.010 0.015 0.6 0.2 0.020 1.2 0.8 0.6 0.4 0.2 10.0 0.02 15.0 0.06 0.02 5.0 -0.02 -0.04 5.0 10.0 10.0 15.0 20.0 e. 72727 y 190.941" no.

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Partl xy plane yz plane zx plane PartBody Pad. 1 tch.l Pad.2 'Sketch.2 pad.3 e Sketch.3 7 Sketch.4 Absolutenxis Geometry.

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A close-up of a computer Description automatically generated with low confidence.

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This involves specifying the following parameters: • Aspect ratio • Taper ratio • Wing sweep • Wing incidence • Dihedral/Anhedral angle. Find geometry of wing planform Calculate the location of the quarter chord of the mean aerodynamic chord.

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Design Activity 7. A picture containing diagram Description automatically generated.

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Results Feedback. WWW:. Overall I was impressed with my results, I manage to complete design activity 1-7 well, I generated more lift and kept tweaking my wings till satisfactory ..

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Thank You very much For your time. A picture containing text, tree Description automatically generated.