Two-Dimensional Subsonic Wind Tunnel Evaluation of Two Related Cambered 15-Percent Thick Circulation Control Airfoils

Abstract

Two circulation control cambered elliptic airfoil sections with a thickness-to-chord ratio of 0.15- and 1.0-percent circular arc camber were evaluated subsonically to determine their aerodynamic characteristics. The two models, designated NCCR 1510-7067N and NCCR 1510-7567S, have a common leading edge but different Coanda surfaces.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1977
Accession Number
ADA055140

Entities

People

  • David W Taylor
  • Jane Abramson

Tags

Communities of Interest

  • Energy and Power Technologies
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Boundaries
  • Boundary Layer
  • Boundary Layer Control
  • Dynamic Pressure
  • Free Stream
  • Geometry
  • High Lift
  • Leading Edges
  • Pressure Distribution
  • Square Roots
  • Stagnation Pressure
  • Static Pressure
  • Subsonic Wind Tunnels
  • Test And Evaluation
  • Two Dimensional
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.