Effects of Mach Number on Maximum Lift

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1947
Accession Number
ADA800815

Entities

People

  • F. N. Kirk

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aircrafts
  • Airfoils
  • Boundary Layer
  • Flow
  • Leading Edges
  • Low Drag
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Gradients
  • Reynolds Number
  • Shock Waves
  • Swept Wings
  • Sweptback Wings
  • Trailing Edges
  • Wind Tunnels