Analytical screening of low emissions, high performance duct burners for supersonic cruise aircraft engines [PDF]
An analytical screening study was conducted to identify duct burner concepts capable of providing low emissions and high performance in advanced supersonic engines. Duct burner configurations ranging from current augmenter technology to advanced concepts
Lohmann, R. A., Riecke, G. T.
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Modelling of jet noise: a perspective from large-eddy simulations. [PDF]
Philos Trans A Math Phys Eng Sci, 2019 Brès GA, Lele SK.
europepmc +1 more source
Integrated control and health management. Orbit transfer rocket engine technology program [PDF]
To insure controllability of the baseline design for a 7500 pound thrust, 10:1 throttleable, dual expanded cycle, Hydrogen-Oxygen, orbit transfer rocket engine, an Integrated Controls and Health Monitoring concept was developed.
Hayden, Warren R., Holzmann, Wilfried A.
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A Historical Systems Study of Liquid Rocket Engine Throttling Capabilities [PDF]
, 2010 This is a comprehensive systems study to examine and evaluate throttling capabilities of liquid rocket engines. The focus of this study is on engine components, and how the interactions of these components are considered for throttling applications ...
Betts, Erin M. +1 more
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Acoustic tests of duct-burning turbofan jet noise simulation [PDF]
The results of a static acoustic and aerodynamic performance, model-scale test program on coannular unsuppressed and multielement fan suppressed nozzle configurations are summarized.
Brausch, J. F. +5 more
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Design and Experimental Study of an Over-Under TBCC Exhaust System. [PDF]
J Eng Gas Turbine Power, 2014 Mo J, Xu J, Zhang L.
europepmc +1 more source
Advanced supersonic propulsion study, phase 3 [PDF]
The variable stream control engine is determined to be the most promising propulsion system concept for advanced supersonic cruise aircraft. This concept uses variable geometry components and a unique throttle schedule for independent control of two flow
Howlett, R. A. +3 more
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Tandem Fan Applications in Advanced STOVL Fighter Configurations [PDF]
The series/parallel tandem fan engine is evaluated for application in advanced STOVL supersonic fighter aircraft. Options in engine cycle parameters and design of the front fan flow diverter are examined for their effects on engine weight, dimensions ...
Eskey, Megan A. +2 more
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Ablative response of a silica phenolic to simulated liquid propellant rocket engine operating conditions [PDF]
Ablative response of silica phenolic to simulated liquid propellant rocket engine operating ...
Moyer, C. B. +3 more
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Proceedings to the 60th Annual Conference of the Particle Therapy Cooperative Group: 27 June - 2 July, 2022, Hosted by Miami Cancer Institute, part of Baptist Health South Florida, Miami, FL, USA. [PDF]
Int J Part Ther, 2023 europepmc +1 more source