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.
Additional Authors:	Grobman, Jack S.
Year:	1957
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/E56I04
Series:	NACA research memorandum ;
Report Number:	E56I04
Subjects:	Air flow
	Charts, diagrams, etc
	Mathematics
	Airplanes--Turbojet engines
	Combustion chambers
Link:	https://hdl.handle.net/2027/mdp.39015086463976