This is a repository of the results of research done on Aerodynamic Performance Characterization of Leading Edge Protrusions on Small Propellers. The paper as well as the data, Labview, arduino, matlab, and solid propeller files are included for future research, collaboration, reference, etc. <div><br></div><div>Licensing for this material is: Attribution 4.0 International (CC BY 4.0) http://creativecommons.org/licenses/by/4.0/ </div><div><br></div><div>Note that several international patents are held by Dr. Frank Fish related to this material, ex: Dewar, S. W., Watts, P., and Fish, F. E., \Turbine and Compressor Employing Tubercle Leading Edge Rotor Design," International patent WO 2006/042401 A1, 2006.</div
This paper deals with preliminary determination of propeller thrust and power coefficients depending...
The work reported in this text describes the development of an advanced method for the aerodynamic t...
[[abstract]]This research experimentally investigates the rotor aerodynamics of horizontal-axis, mic...
The research aims to study the effect of leading edge protuberances on the blade performance at the ...
This thesis presents a Computation Fluid Dynamics (CFD) analysis of the aerodynamic performance of ...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.This...
An experimental study was conducted to examine the flow around swept tapered wings with leading edge...
Leading edge tubercles (LET) is an attractive passive flow control solution that has been proved to ...
This study investigated the effect of leading-edge protuberances on the aerodynamic performance of t...
The paper presents a computational analysis of the characteristics of a NACA 634-021 aerofoil modifi...
This paper reports upon a numerical investigation into the implementation of tubercles in marine pr...
A study has been made on the influence of the leading edge imperfections in airfoils used in differe...
This study implements leading-edge (LE) tubercles on a benchmark 19A accelerating duct to investigat...
The effect of leading-edge geometry on the wake/boundary-layer interaction was studied in a low-spee...
With the recent rise in importance of environmental issues, research on micro hydropower, a kind of ...
This paper deals with preliminary determination of propeller thrust and power coefficients depending...
The work reported in this text describes the development of an advanced method for the aerodynamic t...
[[abstract]]This research experimentally investigates the rotor aerodynamics of horizontal-axis, mic...
The research aims to study the effect of leading edge protuberances on the blade performance at the ...
This thesis presents a Computation Fluid Dynamics (CFD) analysis of the aerodynamic performance of ...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.This...
An experimental study was conducted to examine the flow around swept tapered wings with leading edge...
Leading edge tubercles (LET) is an attractive passive flow control solution that has been proved to ...
This study investigated the effect of leading-edge protuberances on the aerodynamic performance of t...
The paper presents a computational analysis of the characteristics of a NACA 634-021 aerofoil modifi...
This paper reports upon a numerical investigation into the implementation of tubercles in marine pr...
A study has been made on the influence of the leading edge imperfections in airfoils used in differe...
This study implements leading-edge (LE) tubercles on a benchmark 19A accelerating duct to investigat...
The effect of leading-edge geometry on the wake/boundary-layer interaction was studied in a low-spee...
With the recent rise in importance of environmental issues, research on micro hydropower, a kind of ...
This paper deals with preliminary determination of propeller thrust and power coefficients depending...
The work reported in this text describes the development of an advanced method for the aerodynamic t...
[[abstract]]This research experimentally investigates the rotor aerodynamics of horizontal-axis, mic...