Wind-tunnel investigation at low speed of the rolling stability derivatives of a 1/10-scale model of the Douglas A4D-1 airplane: TED No. NACA DE 389
Description:
Report presenting an experimental investigation to determine the low-speed rolling stability derivatives of a scale model of the Douglas A4D-1. The model was tested in clean and landing configurations with horizontal and vertical tails on and off. The data is presented without analysis.
Date:
October 7, 1954
Creator:
Wolhart, Walter D. & Fletcher, H. S.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department