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    A Neural Network Aero Design System for Advanced Turbo-Engines (1999)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: An inverse design method calculates the blade shape that produces a prescribed input pressure distribution. By controlling this input pressure distribution the aerodynamic design objectives can easily be met. Because of the intrinsic relationship between pressure distribution and airfoil physical properties, a neural network can be trained to choose the optimal pressure distribution that would meet a set of physical requirements. The neural network technique works well not only as an interpolating device but also as an extrapolating device to achieve blade designs from a given database. Two validating test cases are discussed.
    Keywords: Aircraft Propulsion and Power
    Type: Air Breathing Engines; Sep 05, 1999 - Sep 10, 1999; Florence; Italy
    Format: application/pdf
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