TEMPERATURE DISTRIBUTION IN THE BOUNDARY LAYER OF AN AIRPLANE WING WITH A LINE SOURCE OF HEAT AT THE STAGNATION EDGE - SYMMETRIC WING IN SYMMETRIC FLOW

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1952
Accession Number
AD0009799

Entities

People

  • Chia-shun Yih
  • Jack E. Cermak
  • Richard T. Shen

Organizations

  • Colorado State University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Boundaries
  • Boundary Layer
  • Civil Engineering
  • Differential Equations
  • Engineering
  • Equations
  • Fluid Mechanics
  • Layers
  • Mechanical Properties
  • Mechanics
  • Military Research
  • Navy
  • Prandtl Number
  • Reynolds Number
  • Stratified Fluids