SOLUTIONS OF THE LAMINAR COMPRESSIBLE BOUNDARY-LAYER EQUATIONS WITH TRANSPIRATION WHICH ARE APPLICABLE TO THE STAGNATION REGIONS OF AXISYMMETRIC BLUNT BODIES

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1959
Accession Number
AD0220332

Entities

People

  • John T. Howe
  • William A. Mersman

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Energy and Power Technologies
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Artificial Intelligence
  • Blunt Bodies
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Differential Equations
  • Equations
  • Flow
  • Fluid Dynamics
  • Heat Transfer
  • Laminar Boundary Layer
  • Mach Number
  • Mass Flow
  • Numerical Analysis
  • Plastic Explosives
  • Skin Friction
  • Two Dimensional