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Key terms: gas flow nozzle using jet km exit mpa pressure velocity exhaust throat supersonic tube gas flow psi mph atm speed constant mass wave isentropic equation gases above fluid solid laval nozzle subsonic values rocket engine expansion ambient becomes venturi absolute temperature operation ideal gas increases combustion propellant mach number flow through compressible supersonic flow linear velocity cross sectional area exhaust gas velocity Search external links cited by footnotes on Wikipedia page De Laval nozzle: |
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