Applications of Hydrofoils with Leading Edge Protuberances

Abstract

The leading edge modified hydrofoils generally create lift equal to or greater than their baseline counterparts at higher angles of attack (beyond the baseline stall angle) whereas at lower angles of attack the baseline models produce lift coefficients equal to or greater than the modified models. The drag coefficients of all modified hydrofoils are either equal to or greater than their baseline counterparts. The relative increase in drag associated with the leading edge protuberances, in turn, results in the lift-to-drag ratio for the modified hydrofoils to be less than or equal to the baseline models. The incipient cavitation numbers for leading edge modified hydrofoils were consistently greater than their their baseline counterparts.

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Document Details

Document Type
Technical Report
Publication Date
Mar 30, 2012
Accession Number
ADA563228

Entities

People

  • Hamid Johari

Organizations

  • California State University, Northridge

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Cameras
  • Cavitation
  • Coefficients
  • Computer-Aided Design
  • Dynamic Pressure
  • Flow Fields
  • Flow Visualization
  • Geometry
  • High Angles
  • High Speed Photography
  • Hydrodynamic Characteristics
  • Hydrofoils
  • Leading Edges
  • Load Cells
  • Measurement
  • Photography
  • Static Pressure

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Marine Propulsion Engineering and Naval Architecture
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