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THRUST CALCULATION [1 record]

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Record 1 2021-01-19

English

Subject field(s)
  • Aerodynamics and Theory of Gases
  • Weapon Systems
OBS

... the classic method of calculating thrust is used by the micropropulsion community to determine nozzle performance from simulation data. This approach accounts for momentum flux and pressure imbalance at the nozzle exit, and it assumes that the viscous stress tensor's contribution to thrust is negligible.

French

Domaine(s)
  • Théorie des gaz et aérodynamique
  • Systèmes d'armes

Spanish

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