THE TRANSVERSE CURVATURE EFFECT IN COMPRESSIBLE AXIALLY-SYMMETRIC LAMINAR BOUNDARY LAYER FLOW

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1954
Accession Number
AD0045752

Entities

People

  • David Elliott
  • Ronald F. Probstein

Organizations

  • Princeton University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Asymptotic Series
  • Boundary Layer
  • Boundary Layer Flow
  • Computational Fluid Dynamics
  • Computational Science
  • Differential Equations
  • Fluid Dynamics
  • Geometry
  • Heat Transfer
  • Hydrodynamics
  • Incompressible Flow
  • Laminar Boundary Layer
  • Mach Number
  • Prandtl Number
  • Two Dimensional
  • Viscous Flow