Results 71 to 80 of about 2,502 (163)

Skylon Aerodynamics and SABRE Plumes [PDF]

open access: yes
An independent partial assessment is provided of the technical viability of the Skylon aerospace plane concept, developed by Reaction Engines Limited (REL).
Afosmis, Michael   +3 more
core   +1 more source

Computer simulation of engine systems [PDF]

open access: yes
The use of computerized simulations of the steady state and transient performance of jet engines throughout the flight regime is discussed. In addition, installation effects on thrust and specific fuel consumption is accounted for as well as engine ...
Fishbach, L. H.
core   +1 more source

Analytical screening of low emissions, high performance duct burners for supersonic cruise aircraft engines [PDF]

open access: yes
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.
core   +1 more source

Modelling of jet noise: a perspective from large-eddy simulations. [PDF]

open access: yesPhilos 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]

open access: yes
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.
core   +1 more source

A Historical Systems Study of Liquid Rocket Engine Throttling Capabilities [PDF]

open access: yes, 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
core   +1 more source

Acoustic tests of duct-burning turbofan jet noise simulation [PDF]

open access: yes
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
core   +1 more source

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