The Stability Derivatives of Low-Aspect-Ratio Triangular Wings at Subsonic and Supersonic Speeds

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1947
Accession Number
ADA801190

Entities

People

  • Herbert S. Ribner

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Airfoils
  • Aspect Ratio
  • Boundary Layer
  • Cartesian Coordinates
  • Coefficients
  • Coordinate Systems
  • Delta Wings
  • Dihedral Angle
  • Flow
  • Leading Edges
  • Lepidoptera
  • Pressure Distribution
  • Skin Friction
  • Trailing Edges
  • Two Dimensional

Technology Areas

  • Hypersonics