ON THE EFFECT OF THICKNESS ON THE DAMPING IN ROLL OF AIRFOILS AT SUPERSONIC SPEEDS

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1953
Accession Number
AD0005479

Entities

People

  • John C. Martin
  • Nathan Gerber

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Airfoils
  • Aspect Ratio
  • Boundaries
  • Delta Wings
  • Differential Equations
  • Equations
  • Free Stream
  • Geometry
  • Leading Edges
  • Mach Number
  • Partial Differential Equations
  • Pressure Distribution
  • Supersonic Flow
  • Swept Wings
  • Three Dimensional
  • Trailing Edges

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow