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Ice Prevention on Aircraft by Means of Engine Exhaust Heat and a Technical Study of Heat Transmission from a Clark Y Airfoil (1933)

NASA Technical Reports Server (NTRS) · leaf 20

An illustration from Ice Prevention on Aircraft by Means of Engine Exhaust Heat and a Technical Study of Heat Transmission from a Clark Y Airfoil, 1933, leaf 20
n pipe is merely a mounting for the support of the model on the airplane. The boiler is of welded sheet iron equipped with a single 3-inch fire tube and is designed to be inserted directly into the exhaust manifold. (Fig. 23.) The length of the boiler is only 3 inches, and its liquid ca- pacity is… … Figure 24.—Experimental installation on airplane of the steam pipe. This gauge was used to assist and the steam line were carefully insulated. The in checking the operation of the system while in water return line runs from the drain cock on flight. the lower left-hand corner of the leading edge…

NASA Technical Reports Server (NTRS)

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