Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas

Author:	Graves, Charles C
Year:	1958
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-1373
Link:	https://digital.library.unt.edu/ark:/67531/metadc60792/