Back to results

Virginia Polytechnic Institute and State University

The effect of free stream disturbances and control surface deflections on the performance of the Wortmann airfoil at low Reynolds numbers

Abstract

dc:description.abstract

A wing with a Wortmann FX-63-137-ESM airfoil section has been used to study some unique problems encountered in wing aerodynamics in the range of Reynolds numbers between 50,000 and 500,000. The wind-tunnel testing conducted in the 6'x 6' Stability tunnel included strain-gauge data, pressure data, and flow-visualization studies. The laminar separation bubble which frequently occurs on the upper surface of the wing is found to dominate its performance and gives rise to a hysteresis loop for lift and drag. Changes in airfoil performance due to positive flap or control surface deflections resemble changes witnessed at higher Reynolds numbers. Negative deflections are seen to considerably change the stall behavior and the flow over the airfoil. This is due to the considerably greater effect on the separation bubble for negative flap deflections. The structure and mechanism of the laminar separation bubble can also be altered by the introduction of selected acoustic disturbance and increased free-stream turbulence. The wind-tunnel test-section environment is, therefore, capable of considerably altering wing performance in this regime.

Degree

thesis:*
Name thesis:degree_name
Ph. D.
Level thesis:degree_level
doctoral
Discipline thesis:degree_discipline
Aerospace Engineering
Department dc:contributor.department
Aerospace Engineering
Grantor dc:publisher
Virginia Polytechnic Institute and State University
Year dc:date.issued
1985

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Sumantran, V.
Chair dc:contributor.committeechair
  • Marchman, James F. III
Committee members dc:contributor.committeemember
  • Schetz, Joseph A.
  • Grossman, Bernard M.
  • Lutze, Frederick H. Jr.
  • Neu, Wayne L.

Rights

dc:rights
Statement dc:rights
  • In Copyright

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/10919/49921
OAI identifier oai:identifier
oai:vtechworks.lib.vt.edu:10919/49921

Chain of custody

source
Harvested from
Virginia Tech
Base URL
vtechworks.lib.vt.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
related terms
citation

Sumantran, V.. The effect of free stream disturbances and control surface deflections on the performance of the Wortmann airfoil at low Reynolds numbers. doctoral thesis, Virginia Polytechnic Institute and State University, 1985. http://hdl.handle.net/10919/49921