A REVIEW OF SOME RECENT PROGRESS IN UNDERSTANDING CATASTROPHIC YAW

Abstract

Catastrophic yaw and roll lock-in are studied at supersonic and subsonic speeds. Roll lock-in is found to occur on isolated fins and is traced to a leading edge vortex. Free rolling motions are found to be accurately represented by the roll lock-in theory. Catastrophic yaw is observed in three- degree-of-freedom and six-degree-of-freedom wind tunnel tests. Mass asymmetry in a 10 degree cone is found to cause rolling velocity, roll lock-in, and catastrophic yaw.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1966
Accession Number
AD0654035

Entities

People

  • John D. Nicolaides

Organizations

  • University of Notre Dame

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Angular Motion
  • Asymmetry
  • Coefficients
  • Errors
  • Flight
  • Flow
  • Fluid Dynamics
  • Free Flight
  • Leading Edges
  • Low Drag
  • National Security
  • Nato
  • Trim Angle
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers