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Conduct Research Top

  • Simulating ice
    is currently upgrading and modifying a Navy S-3 Viking into an icing research platform or IRA (icing-research aircraft). Ice (in white) formed on the leading edge of an airfoil changes the Machnumber contours. The ice shape was obtained by tracing a real ice shape generated in the Icing Research Tunnel
  • Fan Design
    this problem by providing two hub designs for each. series of fan: A smaller structural hub and a properly proportioned. aerodynamic hub referred to as the Air Seal. BLADE SECTION. Structural Hub. The airfoil shape of the fan blade should be selected on the basis. of high efficiency -- that is, high
  • How to Recognize a High-Efficiency Fan
    that. from the thin, narrow tip to the thick cambered root, each section has the proper combination of. airfoil camber, width and angle to provide uniform pressure and velocity from the hub to the tip. This. is the criterion of efficient axial flow fan design. The necessity for uniform flow and pressure

More Information on: Airfoil Section Top

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