Analysis and Calculation by Integral Methods of Laminar Compressible Boundary Layer with Heat Transfer and with and Without Pressure Gradient

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1955
Accession Number
ADA278322

Entities

People

  • Morris Morduchow

Organizations

  • New York University Tandon School of Engineering

Tags

Communities of Interest

  • Air Platforms
  • Biomedical

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Air Force
  • Airfoils
  • Biomedical Research
  • Boundaries
  • Boundary Layer
  • Compressible Flow
  • Critical Temperature
  • Flow
  • Heat Transfer
  • Incompressible Flow
  • Layers
  • Mach Number
  • Pressure Gradients
  • Supersonic Flow
  • United States