Numerical model of viscosity impact on flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with velocity slip
- Authors: Shustov S.A.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 8, No 1 (2009)
- Pages: 79-89
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/636
- DOI: https://doi.org/10.18287/2541-7533-2009-0-1(17)-79-89
- ID: 636
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