Lift Distribution on a High Aspect Ratio Circulation Control Wing with Root Lift Cutout.

Abstract

A computational procedure is developed, based on lifting line theory, which successfully predicts the spanwise lift distribution at moderate blowing momentum coefficient on a high aspect ratio (AR = 18) circulation control wing-body model with several variations in the spanwise lift distribution which validates this procedure. Additional keywords: Coanda surface; Wing body configurations; Mathematical models. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1985
Accession Number
ADA157024

Entities

People

  • David W Taylor
  • R. J. Furey

Tags

Communities of Interest

  • Ground and Sea Platforms
  • Space

DTIC Thesaurus Topics

  • Airfoils
  • Aspect Ratio
  • Boundary Layer
  • Boundary Layer Control
  • Equations
  • Flow
  • Flow Separation
  • Fluid Dynamics
  • Fluid Mechanics
  • Free Stream
  • Geometry
  • Jet Flaps
  • Leading Edges
  • Mathematical Models
  • Potential Flow
  • Pressure Distribution
  • Trailing Edges

Fields of Study

  • Physics

Readers

  • Computational Modeling and Simulation
  • Fluid Mechanics and Fluid Dynamics.
  • Statistical inference.