Forces and moments induced on body of revolution by transverse supersonic jets in transonic and supersonic flow

Wind-tunnel experimental results of aerodynamic normal forces and pitching moments induced on body of revolution by transverse supersonic nonequilibrium jets are shown. The investigations have been carried out for free stream Mach numbers $\rm{M}=0.7,\dots,1.5$, angles of attack $=-10,\dots,+15$ and nozzle expansion ratio $N=0,\dots,450$. Effects of various types of jet blowing on body aerodynamic characteristics are established.