The Design of Cooling Ducts with Special Reference to the Boundary Layer at the Inlet

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1940
Accession Number
ADA801012

Entities

People

  • S. Katzoff

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Boundaries
  • Boundary Layer
  • Drag
  • Duct Inlets
  • Dynamic Pressure
  • Flow
  • Free Stream
  • Fuselages
  • Inlets
  • Layers
  • Measurement
  • Pressure Measurement
  • Resistance
  • Skin Friction
  • Static Pressure
  • Turbulent Boundary Layer