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Published byJerome Martin Modified over 9 years ago
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Flight Simulation: Physics of Aircraft Games Fundamentals © by Jarek Francik Kingston University, London 2012 - 2013
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photo by Arpingstone, Wikimedia Commons
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Main Forces on Aircraft Thrust Weight Lift Drag
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Main Forces on Aircraft Horizontal Forces: Thrust set by Trottle (no formula here)
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Main Forces on Aircraft Horizontal Forces: Thrust set by Trottle (no formula here) Aerodynamic Drag the same formula was used for car simulation! v – air speed – mass density of the air const S p – projected frontal area constC d – drag coefficient
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Main Forces on Aircraft Horizontal Forces: Thrust set by Trottle (no formula here) Aerodynamic Drag the same formula was used for car simulation! v – air speed – mass density of the air const S p – projected frontal area constC d – drag coefficient Drag coefficient is const but may increase with brakes and flaps
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Main Forces on Aircraft Vertical Forces: Weight
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Main Forces on Aircraft Vertical Forces: Weight Lift Force v – air speed – mass density of the air const S w – wing area const C l – lift coefficient
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Main Forces on Aircraft Vertical Forces: Weight Lift Force v – air speed – mass density of the air const S w – wing area const C l – lift coefficient Pilot can control Lift Coefficient
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Lift Force Aerodynamic Drag S p – projected frontal area C d – drag coefficient Lift Force S w – wing area C l – lift coefficient
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Lift Force Source: http://www.lytninslinks.net/physics.htmlhttp://www.lytninslinks.net/physics.html
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Lift Force & Attack Angle FLFL
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FLFL angle of attack Angle of Attack affects: – Lift Coefficient (Lift Force value) – Lift Force direction
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Lift Force & Angle Attack STALL image by Botag, Wikimedia Commons
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Stall Reduction of the Lift Coefficient Occurs when the Critical Attack Angle is exceeded The Critical Angle Attack depends on the speed Two reasons for stall: – too high Angle Attack (typically over 15 o ) – too low speed Very dangerous, used intentionally in some types of aerobatic manoeuvres
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Stall image by US Federal Government, Wikimedia Commons
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Flight Control Systems & Manoeuvres photo by Jarek Francik
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Aircraft Control Pitch Elevator changes Lift Coefficient image: Glen Research Center, NASA, Wikimedia Commons
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Aircraft Control Roll Ailerons imposes Angular Momentum on the Wings image: Glen Research Center, NASA, Wikimedia Commons
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Aircraft Control Roll Ailerons imposes Angular Momentum on the Wings
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Aircraft Control Roll Ailerons imposes Angular Momentum on the Wings image: Glen Research Center, NASA, Wikimedia Commons
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Aircraft Control Yaw Rudder imposes Angular Momentum on the Tail image: Glen Research Center, NASA, Wikimedia Commons
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Aircraft Control More: – Flaps: change drag and lift coefficients, most often used to slow down before landing – Air Brakes: significantly change drag coefficients – Landing Gear – not exactly a flight control system, but will normally affect the drag coefficient – Ground Brakes (used to slow down on the runway)
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Flight Simulator 2D DEMO
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