Vortical thermoregulation systems characteristics calculation

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Vortical pipe geometrical parameters and operation areas calculation is performed. The algorithm counting equal vortical pipes quantity is developed to check the hypothesis that the same vortical pipe can be used with different entrance pressure and temperature parameters to receive necessary cold temperature.

Aircraft, rocket production, vortical effect, aircraft engineering, thermoregulation systems

Короткий адрес: https://sciup.org/148198690

IDR: 148198690

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