Parametric design of non-axisymmetric separate-jet aero-engine exhaust systems
Sign Up to like & getrecommendations! Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.05.038
Abstract: Abstract Future civil air vehicles are likely to feature propulsion systems which are more closely integrated with the airframe. For a podded underwing configuration, this close coupling is expected to require non-axisymmetric design capabilities for… read more here.
Keywords: axisymmetric separate; engine exhaust; aero engine; engine ... See more keywords