Page 36 - Understanding Flight
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CH02_Anderson  7/25/01  8:55 AM  Page 23




                                                                                          How Airplanes Fly 23














                      Fig. 2.5. The variation of the speed of a fluid near an
                      object.




                      The differences in speed in adjacent layers cause shear forces,  The characteristic of fluids to
                      which cause the flow of the fluid to want to bend in the  have zero velocity at the
                      direction of the slower layer. This causes the fluid to try to  surface of an object explains
                      wrap around the object. The characteristic of fluids to have  why one is not able to hose
                      zero velocity at the surface of an object explains why one is  dust off of a car.
                      not able to hose dust off of a car. At the surface of the car the
                      water has no velocity and thus puts little or no force on the dust
                      particles.




                        Viscosity and Lift
                        For those with some familiarity with aerodynamics, there
                        may be some confusion with the connection of viscosity and
                        lift. Many simulations in aerodynamics are done with zero
                        viscosity or, more accurately, in the limit of zero viscosity.
                        Viscosity is introduced implicitly with the Kutta-Joukowski
                        condition, which requires that the air come smoothly off at
                        the trailing edge of the wing. So, in reality these “zero
                        viscosity” calculations reintroduce viscosity via the Kutta-
                        Joukowski condition. In a fluid without viscosity, such as
                        superfluid helium, a wing could not fly.
                        Also, in most mathematical descriptions of lift the boundary
                        layer is considered so small that it is ignored. Many
                        erroneously claim that ignoring the boundary layer is
                        equivalent to having zero viscosity.This is incorrect because
                        viscosity is implicit in the condition that air follows the
                        curvature of the wing.
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