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Linear Motion

Lift Theories. Linear Motion. Requirements for a Valid Theory. A valid theory is a rational explanation of observed phenomenon A valid theory can be used to predict future observations A valid theory produces numerical results. Generation of Lift.

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Linear Motion

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  1. Lift Theories Linear Motion

  2. Requirements for a Valid Theory • A valid theory is a rational explanation of observed phenomenon • A valid theory can be used to predict future observations • A valid theory produces numerical results

  3. Generation of Lift For a lifting airfoil, the surface static pressure varies from top to bottom and from front to back. For a lifting airfoil, the average pressure on the upper surface is lower than the average pressure on lower surface. The difference in pressure produces the lift.

  4. Generation of Lift Why does the surface static pressure vary top to bottom and front to back? The ideal surface velocity varies from top to bottom and front to back. The surface of the foil is a streamline, so Bernoulli’s equation relates the surface velocity to surface pressure. When we include viscosity, the surface velocity is zero, but the local velocity varies at the boundary layer edge.

  5. Generation of Lift Why does the surface velocity vary top to bottom and front to back? The flow must follow the surface contour (or the edge of the boundary layer). Flow can not pass through the airfoil. What determines the values for the local surface velocity, and therefore the local surface pressure, and ultimately the amount of the lift?

  6. Generation of Lift What determines the values for the local surface velocity, and therefore the local surface pressure, and ultimately the amount of the lift? The flow around the airfoil must satisfy the conservation laws: Conservation of mass (continuity) Conservation of momentum (2 or 3 components) Conservation of energy

  7. Euler Equation Solution Uniform Flow + Doublet + Vortex Lift is Generated

  8. Bound Vortex Theory The Kutta Condition Mapped Uniform Flow + Doublet Mapped Uniform Flow + Doublet + Bound Vortex Lift No Lift

  9. Bound Vortex Theory Uniform + Doublet + Bound Vortex G Vortex strength = r Free stream velocity = V r Air density = G V Kutta-Joukowsky Theory r G Lift = L = V Lift Coefficient Theory correctly predicts slope of curve = 2 for thin airfoils p Angle of Attack

  10. Starting (Shed) Vortex

  11. Prandtl’s Experimental Photo of Starting Vortex

  12. Prandtl Lifting Line Theory Bound Vortex Tip Vortex Three dimensional version of Bound Vortex Theory A continuous line of bound vortices terminating at the wing tips with “tip vortices” that continue downstream to the “starting vortex”.

  13. Photo of Tip Vortices

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