Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method

Emanuele RestaRoberto MarsilioMichele Ferlauto2025-04-162025-04-162021jz000105-0271https://tustorage.ulb.tu-darmstadt.de/handle/tustorage/14846530Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control MethodArticlehttps://doi.org/10.3390/fluids6120441