THE INFLUENCE OF TWO-DIMENSIONAL STREAM SHEAR ON AIRFOIL MAXIMUM LIFT

Abstract

The effects of stream velocity gradient on airfoil maximum lift are defined with experimental data obtained in a simulated two-dimensional slipstream.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1961
Accession Number
AD0263597

Entities

People

  • J. H. Hilton
  • J. T. Curtis
  • R. J. Vidal

Organizations

  • Calspan

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aircrafts
  • Boundary Layer
  • Boundary Value Problems
  • Differential Equations
  • Equations
  • Experimental Data
  • Fluid Dynamics
  • Government Procurement
  • Governments
  • Inviscid Flow
  • Laminar Boundary Layer
  • New York
  • Partial Differential Equations
  • Pressure Distribution
  • Shear Flow
  • Viscous Flow

Fields of Study

  • Physics

Readers

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