Approbation of the numerical model of account of viscosity impact on the flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with sliding
- Authors: Shustov S.A.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 8, No 1 (2009)
- Pages: 69-78
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/635
- DOI: https://doi.org/10.18287/2541-7533-2009-0-1(17)-69-78
- ID: 635
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Abstract
The paper outlines the results of approbation of the numerical model developed in [1] of the account of viscosity impact on the flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with sliding by comparing the results of calculations according to the model both with the experimental results and with the results of calculations using a model of a higher level (shortened Navier-Stokes equations in the approximation of a narrow channel).
About the authors
S. A. Shustov
Samara State Aerospace University
Author for correspondence.
Email: vest@ssau.ru
Russian Federation