Title :
New wind tunnel drive control
Author :
Strailman, G. T.
Author_Institution :
Langley Aeronautical Laboratory of the National Advisory Committee for Aeronautics, Langley Field, Va.
fDate :
7/1/1952 12:00:00 AM
Abstract :
With the advent of modern transonic and supersonic aircraft speeds, the size and complexity of wind tunnels to develop designs and evaluate performance has increased enormously. A change in the conventional Kraemer type of control system is presented as a possible solution to the current need.
Keywords :
Commutation; Copper; Liquids; Magnetic tunneling; Reactive power; Rotors; Synchronous motors;
Journal_Title :
Electrical Engineering
DOI :
10.1109/EE.1952.6437597