Accession Number : AD0787459

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

Corporate Author : AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Calarese,Wladimiro

Report Date : JAN 1974

Pagination or Media Count : 165

Abstract : 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)

Descriptors :   *Jet aircraft, *Exhaust nozzles, *Base flow, Afterbodies, Interactions, Transonic airfoils, Problem solving, Theory, Experimental data, Flow fields, Reviews, Subsonic characteristics, Supersonic characteristics, Viscous flow, Inviscid flow, Plumes

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE