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Monterey, California. Naval Postgraduate School

A computational and experimental investigation of the propulsive and lifting characteristics of oscillating airfoils and airfoil combinations in incompressible flow

Abstract

dc:description.abstract

Computational and experimental methods have been used to systematically study one and two airfoils undergoing unsteady motion. first, a single airfoil analysis with the modified computer code, U2DIFF. thrust, efficiency, and phase relationships were computed and compared to existing theoretical results. Furthermore, to help understand the dynamic stall process, relationships were developed between steady and quasi-steady pressure distributions for an airfoil undergoing a ramp motion. Next, an unsteady analysis for two airfoils was done with the modified computer code USPOTF2. Again, thrust and efficiencies for interfering, harmonically oscillating airfoils were computer and compared to existing theoretical results. Furthermore, an analysis was completed on the effects of a harmonically oscillating airfoil on the pressure gradient of a stationary airfoil. Finally, flow visualization experiments were conducted using a low smoke speed tunnel at the Naval Postgraduate School (NPS). This experiment demonstrated the effects of a thrust producing, oscillating airfoil on the formation of the wake vortices. Furthermore, a flow visualization experiment was conducted in the NPS low speed wind tunnel, which demonstrated the beneficial influence of a secondary airfoil oscillating in the vicinity of a stationary airfoil at high-angle-of-attack.

Degree

thesis:*
Department dc:contributor.department
Department of Aeronautics and Astronautics
Grantor dc:publisher
Monterey, California. Naval Postgraduate School
Year dc:date.issued
1992

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Neace, Kerry S.
Advisors dc:contributor.advisor
  • Platzer, Max F.
  • Hebbar, S. K.

Rights

dc:rights
Statement dc:rights
  • This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
Language dc:language.iso
en_US

Identifiers

dc:identifier.*
Handle dc:identifier.uri
https://hdl.handle.net/10945/23578
OAI identifier oai:identifier
oai:calhoun.nps.edu:10945/23578

Chain of custody

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Naval Postgraduate School
Base URL
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Last updated
2026-07-27
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citation

Neace, Kerry S.. A computational and experimental investigation of the propulsive and lifting characteristics of oscillating airfoils and airfoil combinations in incompressible flow. Monterey, California. Naval Postgraduate School, 1992. https://hdl.handle.net/10945/23578