Turbojet and turbofan engine performance increases through turbine burners

Journal of Propulsion and Power

Volumn 17, Issue 3, 2001, Pages 695-705

  Liu, F ^a   Sirignano, W A ^a  

^a UNIVERSITY OF CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTORS; FUEL BURNERS; PRESSURE EFFECTS; THERMOANALYSIS; THERMODYNAMICS; TURBINES;

MACH NUMBER; SPECIFIC THRUST;

TURBOFAN ENGINES;

EID: 0035331013     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5797     Document Type: Article

References (5)

1. Selected challenges in jet and rocket engine combustion research
2. Performance increases for gas turbine engines through combustion inside the turbine
3. Diffusion flame in a two-dimensional, accelerating mixing layer
4. Ignition and flame studies for an aceelerating transonic mixing layer