Analysis of Circulation Controlled Airfoils

Abstract

A self-contained analysis for arbitrary circulation controlled airfoils in incompressible flow is developed. The analysis predicts the blowing slot conditions required to produce a specified lift coefficient on a given airfoil with given free stream conditions. An iterative procedure is used to find the blowing slot conditions that allow the Thwaites condition of constant pressure in the separated region to be satisfied. With the input given, a potential flow analysis is performed using the Theodorsen method. Boundary layer analyses for the lower and upper surfaces then yield the separation pressure on the lower surface and the boundary layer properties at the slot on the upper surface. The flow is initially laminar and usually becomes turbulent. The Cebeci, Smith finite difference method is used and an eddy viscosity model is used for turbulent flow. Blowing slot values are assumed and a turbulent wall jet analysis is performed to determine the wall pressure at separation on the upper surface.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1975
Accession Number
ADA013334

Entities

People

  • Edward H. Gibbs
  • Nathan Ness

Organizations

  • West Virginia University

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Boundary Layer
  • Channel Flow
  • Crystal Structure
  • Experimental Data
  • Fluid Dynamics
  • Free Stream
  • Geometry
  • Incompressible Flow
  • Military Research
  • Potential Flow
  • Pressure Distribution
  • Pressure Gradients
  • Shear Stresses
  • Turbulent Flow
  • Two Dimensional
  • United States
  • West Virginia

Fields of Study

  • Physics

Readers

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