Abstract
The firing of rockets from launchers is accompanied by strong jet-wall interactions. So-called non-tip launchers, which have changes in cross-sectional areas, produce especially complicated flow patterns with massive blow-by over the missile body suspected to cause initial trajectory degradation. A comprehensive analysis for this launch phase is presented which delineates component flow mechanisms, subsequently integrating them into an overall model with the solution obtained by a convergent process of iterations. Since the analysis is free of empirical input, it provides a firm basis for comparison with available experimental data. Quantitative agreement between theoretical and experimental results not only supports the correctness of the overall physical model and its mathematical simulation, but also allows the designer to explore the effects of individual design and operational parameters.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
