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Investigation of Gas-Turbine Afterburner with Aluminized Fuel-Rich Propellant
P Nema, A Bhadran, S Shanmugam… - Journal of Propulsion …, 2025 - arc.aiaa.org
This paper describes the design and development of a compact afterburner system for a
mini gas turbine engine using aluminized fuel-rich propellant. The working principle of the …
mini gas turbine engine using aluminized fuel-rich propellant. The working principle of the …
The shape and dimensions of flame stabilizers of a direct-flow type combustion chamber influence on the hydraulic characteristics
D Kozel - Aerospace Technic and Technology, 2022 - nti.khai.edu
Direct-flow combustion chambers are afterburner combustion chambers, which are used to
short-term increase the thrust of a gas turbine engine for takeoff, maneuvering and …
short-term increase the thrust of a gas turbine engine for takeoff, maneuvering and …