Comparison of Yaw Characteristics of a Single-Engine Airplane Model With Single-Rotating and Dual-Rotating Propellers
Description:
Report presenting testing in the pressure tunnel to determine the yaw characteristics of a scale model of a single-engine, fighter-type airplane with six-blade single-rotating and dual-rotating propellers. Force and moment characteristics are presented for several model and power conditions.
Date:
April 1944
Creator:
Neely, R. H.; Fogarty, L. E. & Alexander, S. R.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department