Some Recent Research on Airfoil Dynamic Stall with Application to Airfoil Design,

Abstract

Some recent research on airfoil dynamic stall tentatively defines the boundary-layer flow processes during dynamic stall and suggests an approach to airfoil design for stall delay. The effect of changes of airfoil leading-edge radius and camber on increments in maximum lift coefficients is estimated, using a simple criterion for leading-edge stall. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1971
Accession Number
AD0734699

Entities

People

  • Norman D. Ham

Organizations

  • Massachusetts Institute of Technology

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Boundary Layer Flow
  • Coefficients
  • Flow
  • Leading Edges

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Defense Acquisition Program Management