A preliminary investigation of the icing characteristics of a large rectangular-throat pressure-type carburetor

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086 0 ‡aY 3.N 21/5:11/E284
088 ‡aNACA MR E6G11
088 ‡aNACA WR E284
100 1 ‡aChapman, Gilbert E.
245 1 2 ‡aA preliminary investigation of the icing characteristics of a large rectangular-throat pressure-type carburetor / ‡cGilbert E. Chapman.
246 1 3 ‡aNACA Wartime Reports. Series E.
260 ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c[1946].
300 ‡a6, [5] p. : ‡bill. ; ‡c27 cm.
490 0 ‡aWartime Report / National Advisory Committee for Aeronautics ; ‡vno. E284
500 ‡aPrepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio.
500 ‡aOriginally issued as NACA as Memorandum Report E6G11 (July 1946).
500 ‡aNACA Wartime Report E-284.
504 ‡aIncludes bibliographical references.
520 3 ‡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.
538 ‡aMode of access: Internet.
650 0 ‡aAirplanes ‡xIce formation.
650 0 ‡aAirplanes ‡xMotors ‡xCarburetors.
710 2 ‡aAircraft Engine Research Laboratory.
710 1 ‡aUnited States. ‡bNational Advisory Committee for Aeronautics.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
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