FUNDAMENTALS OF THE STABILITY OF PERIPHERAL JET VEHICLES. EFFECT OF JET THICKNESS,

Abstract

Contents: Total Head and Cushion Pressure-general relation, vortex theory, exponential theory, quasi-thin theory, discussion of theories, approximation for very thin jets; The Vortex Theory Jet--calculation of jet-form parameter, velocity and pressure distribution, mass and momentum flux, comparison with simple momentum theory, O'Neill's functions; Illustrating a Danger in Interpreting Published Test Results-Crewe's epsilon, Overfed Operation - Quasi-Thin Jet Theory, Overfed Operation - Vortex Jet Theory, Underfed Operation; contraction ratio for an infinitely thin jet, and contraction ratio for a quasi-thin jet and a vortex-theory jet.

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1963
Accession Number
AD0425570

Entities

People

  • M. C. Eames

Tags

DTIC Thesaurus Topics

  • Geometry
  • Momentum
  • Physical Properties
  • Pressure Distribution
  • Thickness

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Combustion Dynamics and Shock Wave Physics.
  • Fluid Mechanics and Fluid Dynamics.