Record Details

Electrolytic simulation of airfloil flow

ScholarsArchive at Oregon State University

Field Value
Title Electrolytic simulation of airfloil flow
Names Sworakowski, Michael Thomas (creator)
Stone, Louis N. (advisor)
Date Issued 1963-08-07 (iso8601)
Note Graduation date: 1964
Abstract Airfoil flow simulation tests were carried out in a 20-inch
diameter double layer circular electrolytic tank. Results of the
tests indicate that the tank very closely approximates ideal conditions.
The double layer circular electrolytic tank is shown to
generate a very large rectangular tank. Formulas were derived to
show that this double layer tank is valid for the analogy between
fluid velocity and voltage gradient.
Tests were performed on a five inch diameter cylindrical
model. The first series of tests was performed with the ground
plane very far from the model surface. Electrical current to the
model was adjusted so that circulation and lift could be calculated
for different angles of stagnation point on the model.
The second series of tests was performed with suitable
electrodes so the model would be near the ground plane. The purpose
of these tests was to investigate how circulation, lift, and effective velocity varied when model to ground plane distance was
varied.
The appendix contains data in a format similar to that in
which it was used in the ALWAC IIIE computer to obtain numerical
results. AIso in the appendix are results of investigations on circular
airfoils made by other investigators using conducting sheets
and a wind tunnel.
A discussion of equipment used and improvements that
could be made is included.
Genre Thesis/Dissertation
Topic Aerodynamics -- Electromechanical analogies
Identifier http://hdl.handle.net/1957/48716

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