Effects of fuel-nozzle carbon deposition on combustion efficiency of single tubular-type, reverse-flow turbojet combustor at simulated altitude conditions

Author:	Dittrich, Ralph T
Year:	1948
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-1618
Link:	https://digital.library.unt.edu/ark:/67531/metadc54798/