Simulation of gas flow and heat transfer in supersonic nozzle
Aerospace propulsion engineering
Аuthors
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
e-mail: bykovlv@mai.ru
Keywords:
Convective heat transfer; supersonic turbulent flows; liquid rocket jets; heat transfer coefficient; thermal protectionDownload