GENERALIZED MISSILE DYNAMICS ANALYSIS. III. AERODYNAMICS,

Abstract

The aerodynamic forces acting on a missile in consequence of small perturbations from a prescribed trajectory are calculated on the basis of slender body theory and piston theory is applied, in some detail, to the specific example of Generalized Missile Dynamics Analysis, II Equations of Motion.

Document Details

Document Type
Technical Report
Publication Date
Apr 07, 1958
Accession Number
AD0607552

Entities

People

  • Dana Young
  • J. W. Miles

Organizations

  • TRW Inc.

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Forces
  • Aerodynamics
  • Bodies
  • Computational Fluid Dynamics
  • Computational Science
  • Dynamics
  • Equations
  • Equations Of Motion
  • Fluid Dynamics
  • Fluid Mechanics
  • Mathematics
  • Mechanics
  • Perturbations
  • Slender Bodies

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Control Systems Engineering.