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1Sensitivity analysis for aeroacoustic and aeroelastic design of turbomachinery blades

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“Sensitivity analysis for aeroacoustic and aeroelastic design of turbomachinery blades” Metadata:

  • Title: ➤  Sensitivity analysis for aeroacoustic and aeroelastic design of turbomachinery blades
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Dept. of Mechanical Engineering and Materials Science, School of Engineering, Duke University
  • Publish Date:
  • Publish Location: ➤  Durham, NC - [Washington, DC - Springfield, Va

“Sensitivity analysis for aeroacoustic and aeroelastic design of turbomachinery blades” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1995
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    Wiki

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    Computational fluid dynamics

    coupled boundary layer codes for airfoil analysis work. PROFILE uses a conformal transformation method for inverse airfoil design, while XFOIL has both a

    Shock wave

    In the examples below, the shock wave is controlled, produced by (ex. airfoil) or in the interior of a technological device, like a turbine. These shocks

    Cathleen Synge Morawetz

    mathematics of transonic flow, she showed that specially designed shockless airfoils could not, in fact, prevent shocks. Shocks developed in response to even

    Boundary layer

    the boundary layer in the direction normal to the surface (such as an airfoil) remains relatively constant throughout the boundary layer, and is the

    Glossary of aerospace engineering

    generated by an airfoil to the speed of the airfoil through the fluid, the density of the fluid and the circulation around the airfoil. The circulation

    Dimensionless numbers in fluid mechanics

    {U} ={\frac {H\,\lambda ^{2}}{h^{3}}}} Fritz Ursell wave mechanics (nonlinearity of surface gravity waves on a shallow fluid layer) Wallis parameter j∗

    Wind turbine design

    turbines can survive 80 metres per second (290 km/h; 180 mph). A stall on an airfoil occurs when air passes over it in such a way that the generation of lift

    Index of physics articles (N)

    Nonlinear photonic crystal Nonlinear resonance Nonlinear Schrödinger equation Nonlinear system Nonlinear X-wave Nonlinearity (journal) Nonlocal Lagrangian

    Aileron

    the aircraft's wings. Aileron struts combined movable surfaces with an airfoil shaped wing strut. Acting in the propeller slipstream increased their effectiveness

    Multi-objective optimization

    systems in the circumstances such as control cabinet layout optimization, airfoil shape optimization using scientific workflows, design of nano-CMOS, system