Psuedo-Shock as a Qualitative Model in the Investigation of the Influence of Wall Roughness on the Performance of Supersonic MHD Generators.

Abstract

A preliminary study, based on an extension of Crocco's pseudo-shock model, has been carried out to explain and predict qualitatively the rather gradual pressure rise in a supersonic MHD generator, to account for the influence of wall roughness on the core flow. A system of non-linear ordinary differential equations is formulated for the wall layer and core, with proper electromagnetic conditions enforced at the interface. Extensive numerical experiments are also presented, which demonstrate indeed the qualitative link between the theory of MHD pseudo-shock and the observed pressure ramp caused by rough walls. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1980
Accession Number
ADA088333

Entities

People

  • Pau-chang Lu

Organizations

  • University of Nebraska-Lincoln Department of Mechanical and Materials Engineering

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Channel Flow
  • Conductivity
  • Differential Equations
  • Engineering
  • Equations
  • Gas Laws
  • Generators
  • Heat Capacity
  • Heat Transfer
  • Ideal Gas Law
  • Lorentz Force
  • Magnetic Fields
  • Mechanical Engineering
  • Specific Heat
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow