Effect of flame stabilizer design on performance and exhaust pollutants of a two-row 72-module swirl-can combustor

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050 4 ‡aTL521.3 ‡b.A33 no.3373
086 0 ‡aNAS 1.15:X-3373
100 1 ‡aBiaglow, James A.
245 1 0 ‡aEffect of flame stabilizer design on performance and exhaust pollutants of a two-row 72-module swirl-can combustor / ‡cJames A. Biaglow and Arthur M. Trout.
260 ‡aWashington : ‡bNational Aeronautics and Space Administration, Lewis Research Center ; ‡eSpringfield, Va. : ‡ffor sale by the National Technical Information Service, ‡c1976.
300 ‡a21 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNASA technical memorandum ; NASA TM X-3373
538 ‡aMode of access: Internet.
650 0 ‡aCombustion ‡xResearch.
650 0 ‡aAircraft exhaust emissions.
650 0 ‡aAir ‡xPollution.
650 0 ‡aAirplanes ‡xTurbojet engines ‡xCombustion.
700 1 ‡aTrout, Arthur M., ‡ejoint author.
CID ‡a011426005
DAT 0 ‡a20101006143353.0 ‡b20141013010000.0
DAT 1 ‡a20141112173021.0 ‡b2025-01-01T19:14:54Z
DAT 2 ‡a2025-01-01T18:30:02Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ‡aBK
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