Review of Methods of Solution of Afterbody/Exhaust Nozzle Flow Fields,

摘要

A review is made of methods of solution for afterbody/exhaust nozzle flow fields in different flight regimes. For the transonic regime airfoil solutions are also presented. A comparison between various theories and experiments is made wherever considered necessary to show the state-of-the-art. Most of the available theories are selected and correlated. (Author)