An Inverse Boundary-Layer Method for Compressible Laminar and Turbulent Flows

Abstract

This report presents an efficient method for calculating laminar and turbulent boundary-layer flows for standard and inverse boundary-value problems. It is applicable to both incompressible and compressible flows. The standard boundary-layer problem considers the solution of the usual boundary-layer equations for a given external velocity distribution. The inverse problem considers the solution of the governing equations for assigned wall shear or assigned displacement thickness.

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Document Details

Document Type
Technical Report
Publication Date
Apr 08, 1975
Accession Number
ADA010270

Entities

People

  • Tuncer Cebeci

Organizations

  • California State University, Long Beach

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Boundary Layer
  • Boundary Layer Flow
  • Computational Science
  • Difference Equations
  • Differential Equations
  • Equations
  • Fluid Dynamics
  • Laminar Boundary Layer
  • Leading Edges
  • Mach Number
  • Mechanical Engineering
  • Navier Stokes Equations
  • Pressure Gradients
  • Turbulent Boundary Layer
  • Turbulent Flow
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.