Gaseous exhaust emissions from a J-58 engine at simulated supersonic flight conditions [PDF]
Emissions of total oxides of nitrogen, unburned hydrocarbons, carbon monoxide, and carbon dioxide from a J-58 engine at simulated flight conditions of Mach 2.0, 2.4, and 2.8 at 19.8 km altitude are reported.
Holdeman, J. D.
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Impact of Biofuel Blends on Black Carbon Emissions from a Gas Turbine Engine. [PDF]
Energy Fuels, 2020 Kumal RR +19 more
europepmc +1 more source
Bibliography on aerodynamics of airframe/engine integration of high-speed turbine-powered aircraft, volume 1 [PDF]
This bibliography was developed as a first step in the preparation of a monograph on the subject of the aerodynamics of airframe/engine integration of high speed turbine powered aircraft.
Nichols, M. R.
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Application of real-time engine simulations to the development of propulsion system controls [PDF]
The development of digital controls for turbojet and turbofan engines is presented by the use of real-time computer simulations of the engines. The engine simulation provides a test-bed for evaluating new control laws and for checking and debugging ...
Szuch, J. R.
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Diagnostics of three-shaft turbojet two-circuit engine by using the dynamic parameters
, 1998 Є. М. Карпов, Artem Karpov
openalex +2 more sources
Design Point Parameter Estimation of a Legacy Twin Spool Turbojet Engine for Health Monitoring
, 2023 Balaji Sankar +5 more
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Gear-Shaped High-g Combustion Chamber for Micro Turbojet Engine Applications. [PDF]
ACS OmegaHuang H, Chen G, Long H, Lei B, Liang J.
europepmc +1 more source
Parametric Damage Mechanics Empowering Structural Health Monitoring of 3D Woven Composites. [PDF]
Sensors (Basel), 2023 Jacot M +3 more
europepmc +1 more source
Toward a second generation fuel efficient supersonic cruise aircraft performance characteristics and benefits [PDF]
The need for greatly improved fuel efficiency and off-design subsonic characteristics is discussed. Engine-airframe matching studies are presented which show the benefits of a configuration designed for much lower supersonic drag levels (blended wing ...
Vachal, J. D.
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