Abstract
This paper uses three-dimensional dynamical simulation of gas jet to demonstrate basic deflecting features of the double-faced deflector, during the launch process of the land-based missile with the vehicle-mounted vertically thermal launch. The calculation shows that the deflection of the gas flow is good, reducing knock-on effect and ablative effect on launch device. But wheels of the launch vehicle are still under visible influent from the gas flow. The paper optimizes the double-faced deflector and compares different suggestions in order to find a better deflection.
Original language | English |
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Title of host publication | Applied Mechanics, Materials and Mechanical Engineering |
Pages | 314-318 |
Number of pages | 5 |
DOIs | |
Publication status | Published - 2013 |
Event | 2013 International Conference on Applied Mechanics, Materials and Mechanical Engineering, AMME 2013 - Wuhan, China Duration: 24 Aug 2013 → 25 Aug 2013 |
Publication series
Name | Applied Mechanics and Materials |
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Volume | 387 |
ISSN (Print) | 1660-9336 |
ISSN (Electronic) | 1662-7482 |
Conference
Conference | 2013 International Conference on Applied Mechanics, Materials and Mechanical Engineering, AMME 2013 |
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Country/Territory | China |
City | Wuhan |
Period | 24/08/13 → 25/08/13 |
Keywords
- Double-faced deflector
- Gas jet
- Launching dynamics
- Numerical simulation
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Shi, S. Y., Jiang, Y., & Dong, X. T. (2013). Deflecting features of gas from double-faced deflector and structure optimization of deflector. In Applied Mechanics, Materials and Mechanical Engineering (pp. 314-318). (Applied Mechanics and Materials; Vol. 387). https://doi.org/10.4028/www.scientific.net/AMM.387.314