Collocation Flutter Analysis Study II (COFA II). Volume 1. Subsonic Strip Theory Unsteady Aerodynamics Program. Supersonic Piston Theory Unsteady Aerodynamics Program

Abstract

The work presented in this report is a continuation of work started under NASC Contract No. 00019-68-C-0274, Collocation Flutter Analysis Study. This work, which is presented in three volumes, is to update and document computer automated flutter analysis techniques. This volume contains subsonic strip theory unsteady aerodynamics program (Strip), and supersonic piston theory unsteady aerodynamics program (Piston).

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1970
Accession Number
AD0872190

Entities

Organizations

  • Hughes Aircraft Company

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Aerodynamics
  • Aspect Ratio
  • Computer Programs
  • Computers
  • Control Surfaces
  • Flow
  • Fluid Dynamics
  • Frequency
  • Geometry
  • Instructions
  • Mach Number
  • Plastic Explosives
  • Standards
  • Steady State
  • Trailing Edges
  • Unsteady Aerodynamics

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Computer Science.
  • Technical Research and Report Writing.

Technology Areas

  • Hypersonics