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110302s1946 dcua tb f000 0 eng d |
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‡a(MiU)990139479530106381
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‡aMAIN
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‡aY 3.N 21/5:11/E284
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‡aNACA MR E6G11
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‡aNACA WR E284
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‡aChapman, Gilbert E.
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‡aA preliminary investigation of the icing characteristics of a large rectangular-throat pressure-type carburetor /
‡cGilbert E. Chapman.
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‡aNACA Wartime Reports. Series E.
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‡aWashington, D.C. :
‡bNational Advisory Committee for Aeronautics,
‡c[1946].
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‡a6, [5] p. :
‡bill. ;
‡c27 cm.
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‡aWartime Report / National Advisory Committee for Aeronautics ;
‡vno. E284
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‡aPrepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio.
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‡aOriginally issued as NACA as Memorandum Report E6G11 (July 1946).
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‡aNACA Wartime Report E-284.
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‡aIncludes bibliographical references.
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‡aA rectangular-throat pressure-type carburetor was investigated to determine the icing characteristics of this part of a large four-engine bomber induction system. Runs of 15-minute duration were made at a simulated low-cruising power condition over a range of carburetor-air temperatures from 12 to 100 degrees F with varied moisture contents to establish the limiting conditions for the formation of visible and serious icing. The investigation included icing tests made with a standard nozzle bar and an impinging-jets nozzle bar.
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‡aMode of access: Internet.
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‡aAirplanes
‡xIce formation.
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‡aAirplanes
‡xMotors
‡xCarburetors.
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‡aAircraft Engine Research Laboratory.
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‡aUnited States.
‡bNational Advisory Committee for Aeronautics.
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‡aTechnical Report Archive & Image Library (TRAIL)
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899 |
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‡a39015095014620
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‡b20221206000000.0
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‡a20221210140713.0
‡b2024-04-02T17:44:42Z
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