Zobrazeno 1 - 2
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pro vyhledávání: '"Amar Gandge"'
Publikováno v:
International Review of Aerospace Engineering; Dec2023, Vol. 16 Issue 6, p233-245, 13p
Publikováno v:
Journal of Mines, Metals and Fuels. 69:234
Rocket nozzle is part of a rocket in which the burnt propellant from the combustion chamber can exhaust through the nozzle to get the desire amount of thrust and required Mach number. The nozzle turns the static high pressure high temperature gas to