作者: Jackie Raymond Julien Prouteau , Thomas Daris , Alain Pierre Page , Edgar Brunet
DOI:
关键词: Propulsion 、 Nozzle 、 Gas generator 、 Mechanics 、 Duct (flow) 、 Engineering 、 Aerospace engineering
摘要: A propulsion gas exhaust assembly is presented for use in an aircraft propelled by hot gases produced along the axis of latter a generator. The may include first cylindrical duct, two second ducts, third and axial gas-ejection nozzles. duct element receives downstream gasses flow from to elements. These elements are divergent geometric plane. Each guide their own respective nozzle. ducts elbows assist stealth. nozzles means steer aircraft.