Cooling of airplane engines at low air speeds
Description:
Report presents the results of a comprehensive experimental study carried out at full scale in the NACA 20-foot wind tunnel, the general purpose of which is to furnish information in regard to the functioning of the power plant and propeller unit under different conditions. This report deals particularly with the problem of the cooling of an airplane engines on the ground. The influence of different nose forms, skirts, flaps, propellers, spinners, and special blowers has been investigated.
Date:
June 2, 1936
Creator:
Theodorsen, Theodore; Brevoort, M. J. & Stickle, George W.
Item Type:
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Partner:
UNT Libraries Government Documents Department