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- W747701788 abstract "E requirements for heated pitot static tubes for the operation of air-speed indicators were subordinate to the greater problem of ice accumulation on the lifting surfaces of the airplane. The purpose of pitot tube heating was merely that of delaying ice formation thereon so as to insure operation of the airspeed indicator as long as the airplane could fly. But when devices which removed ice continuously from wing and tail surfaces permitted sustained flight under adverse conditions, it became necessary that the air-speed indicator should operate at all times. The first electrically heated pitot static tubes commercially available had a heating element consuming approximately 50 watts, based on the rather limited information then available. In 1937, some serious tests were initiated by the Army Air Corps and by United Air Lines, using the facilities of the B. F. Goodrich Company in whose refrigerated wind tunnel (Fig. 1) experiments can be carried out under severe ice-forming conditions." @default.
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- W747701788 date "1938-08-01" @default.
- W747701788 modified "2023-09-27" @default.
- W747701788 title "Icing of Pitot Static Tubes" @default.
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- W747701788 doi "https://doi.org/10.2514/8.678" @default.
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