Collocation Flutter Analysis Study II (COFA II). Volume 2. Unsteady Aerodynamic Generalized Force Programs for Subsonic, Transonic, and Supersonic Flight Regimes

Abstract

This volume presents three computer programs that calculate the generalized aerodynamic forces for the three flight regimes: Subsonic Flight, Transonic Flight, Supersonic Flight and may be used with the Modal Flutter Analysis Program of Vol. III. The subsonic program is based upon Kernel Function formulation. The transonic and supersonic programs are based upon the Mach Box technique.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1970
Accession Number
AD0872180

Entities

Organizations

  • Hughes Aircraft Company

Tags

Communities of Interest

  • Advanced Electronics
  • C4I
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Acoustic Velocity
  • Aerodynamic Forces
  • Computer Programs
  • Computers
  • Control Surfaces
  • Equations
  • Frequency
  • Integral Equations
  • Kernel Functions
  • Leading Edges
  • Lifting Surfaces
  • Mach Number
  • Operating Systems
  • Plastic Explosives
  • Pressure Distribution
  • Supersonic Flight
  • Unsteady Aerodynamics

Fields of Study

  • Physics

Readers

  • Computer Science.
  • Control Systems Engineering.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics