Maneuverable missile and turbofan engine integrated design constrain analysis and mission analysis
By using the method of aircraft and turbofan engine integrated analysis,a model of maneuverable missile and turbofan engine integrated constrain analysis and mission analysis was developed and the computative examples and the analysis were given.The mission section,the constrain conditions,the weight composition of the maneuverable missile,and the model of used in turbofan engine maneuverable missile were presented.A prediction method of lift to drag ratio of subsonic maneuverable missile was given.The empty weight to total weight ratio of subsonic maneuverable missile was given experimentally.The constrain analyzed results and the mission analyzed results of some maneuverable missiles indicate that the model of maneuverable missile and turbofan integrated constrain analysis and mission analysis is feasible and available.