Analysis of aerodynamic/propulsive couplings during mode transition of over-under turbine-based-combined-cycle engines
Sign Up to like & getrecommendations! Published in 2020 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2020.105773
Abstract: Abstract Mode transition control is a critical issue of a Turbine-Based-Combined Cycle (TBCC) engine when the main thrust provider changes from a gas turbine engine to a scramjet engine. Compared with a scramjet-powered integrated aircraft,… read more here.
Keywords: transition; turbine based; control; mode transition ... See more keywords