Effect of Turbulent Jet Mixing on the Static Lift Performance of a Power Augmented Ram Wing,

Abstract

Calculation procedures are developed using axisymmetric and two dimensional turbulent jet theory for predicting the static lift performance of a two dimensional power augmented ram wing. The resulting lift prediction is found to be in good agreement with experimental data. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1977
Accession Number
ADA049620

Entities

People

  • Basil S. Papadales Jr.
  • David W Taylor
  • Harvey R. Chaplin
  • William J. H. Smithey

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Agreements
  • Air Entrainment
  • Axisymmetric
  • Boundary Layer
  • Dynamic Pressure
  • Entrainment
  • Equations
  • Experimental Data
  • Flow
  • Fluid Dynamics
  • Ground Effect
  • Leading Edges
  • Mixing
  • Momentum
  • Thickness
  • Turbulent Mixing
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Mechanics and Fluid Dynamics.