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Published February 1951 | Submitted
Journal Article Open

Design and Performance of a Simple Interferometer for Wind Tunnel Measurements

Abstract

The design of an interferometer with a 3 1/2" diameter light field and its application to a continuously operating 4" x 10" supersonic wind tunnel are discussed. The main features of this interferometer are (1) its very law cost compared to previous designs, (2) its light weight and flexibility, (3) a simple device permitting the instrument to be used also as a Schlieren system, and (4) its unique feature of passing both light beams through the test section to minimize the effect of the side wall boundary layers in the interferograms.

Additional Information

© 1951 Institute of the Aeronautical Sciences. Received June 12, 1950.

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August 19, 2023
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