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Numerical Computation of Specific Impulse and Internal Flow Parameters in Solid Fuel Rocket Motors with Two-Phase Сombustion Products
Authors: Sultanov T.S., Glebov G.A. | Published: 08.09.2021 |
Published in issue: #3(138)/2021 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: solid propellant rocket engines, numerical methods, two-phase flows, specific impulse, supersonic nozzle |