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  1. Chapter 5: Theory of Airfoil Lift Aerodynamics – Intermediate Aerodynamic Theory and Analysis. 5 Chapter 5: Theory of Airfoil Lift Aerodynamics. Airfoil theory is largely governed by potential flow theory. Specifically, a key component of airfoil aerodynamics theory is the combination of: Free-stream velocity elementary flow.

    • Lift
    • Factors of Flow
    • Lift Equation

    All that is necessary to create lift is to turn a flow of air. An aerodynamic, curved airfoil will turn a flow. But so will a simple flat plate, if it is inclined to the flow. The fuselage of an airplane will also generate lift if it is inclined to the flow. For that matter, an automobile body also turns the flow through which it moves, generating ...

    There are many factors that affect the turning of the flow, which creates lift. We can group these factors into(a) those associated with the object, (b) those associated with the motion of the object through the air, and (c) those associated with the air itself: 1. Object:At the top of the figure, aircraft wing geometry has a large effect on the am...

    We can gather all of this information on the factors that affect lift into a single mathematical equation called the Lift Equation. With the lift equation we can predict how much lift force will be generated by a given body moving at a given speed.

    • The Four Forces Acting on an Airplane. DESIGN PARAMETER: Wing (Airfoil) GEOMETRY/STRUCTURE: The airplane generates lift using its wings. The cross-sectional shape of the wing is called an airfoil.
    • Typical Airfoli (Cross-Sectional Shape) of An Airplane Wing. Chord: Extends from leading edge to trailing edge of the wing. Camber line: Points halfway between chord and upper wing surface.
    • A Few Different Airfoils. Note: There Are An Infinite Number of Possibilities; i.e. a) Flat Bottom; b) Slightly Curved Bottom; c) Symmetrical. Viscosity is essential in generating lift.
    • Starting Vortex Formation. As shown in Figure 4, the starting vortex rotates in a counter-clockwise direction. To satisfy the conservation of angular momentum, there must be an equivalent motion to oppose the vortex movement.
  2. Jan 25, 2012 · Now, University of Cambridge’s Professor Holger Babinsky has created a 1-minute video that he hopes will finally lay to rest a commonly used yet misleading explanation of how wings lift. “A wing lifts when the air pressure above it is lowered. It’s often said that this happens because the airflow moving over the top, curved surface has a ...

  3. Jul 5, 2019 · So, according to Newton's third law, the air also should push the airfoil in opposite direction with equal magnitude. This results in lift. Fig 12 : Newton's third law of motion. In conclusion, the deflection or curvature of the flow caused by the Coanda effect generates the lift.

  4. The best-performing airfoil in our test studies had a suction side vertex at 33% chord length, pressure side vertex at 67%, suction side thickness at 14%, and pressure side thickness at 8.5%. This combination produced a lift-drag ratio of 48. The flow field for this airfoil is displayed in Fig.6.

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  6. Tilting the wing upward (or increasing the angle of attack) increases lift—to a point—but decreases airspeed. If you tilt it too much, the airflow pulls away from the upper surface, and the smooth flow turns turbulent. The wing suddenly loses lift, a condition known as a stall. You can reestablish a smooth airflow by tilting the wing back ...

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