Performance of an annular turbojet combustor having reduced pressure losses and using propane fuel Page: 1 of 40
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S.A i-l I Y IIJ r I-MA - ION
, s ASSIFIED CONFIDENTIAL
LANGLE AtCPONAUELAL L JtAIURY
PERFORMANCE OF AN ANNULAR TURBOJET COMBUSTOR HAVING
REDUCED PRESSURE LOSSES AND USING PROPANE FUEL
By Carl T. Norgren and J. Howard Childs
Lewis Flight Propulsion Laboratory
Uy tuthoti ty GEOf.Date1SJ1Q7
CL88IED 1 CU2
This material contains I nfrmation affecting ts Ntional Defense of the United States within the meaning
of theim s418,UA%&.0) Seo 798Ua & R, the transmission or revelattIn of which In any
manner u Dorisd person is prohibited by law.
NATIONAL ADVISORY COMMITTEE
September 24, 1953 N A C A LIBKARY
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Norgren, Carl T. & Childs, J. Howard. Performance of an annular turbojet combustor having reduced pressure losses and using propane fuel, report, September 24, 1953; (https://digital.library.unt.edu/ark:/67531/metadc59759/m1/1/: accessed April 20, 2019), University of North Texas Libraries, Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.