Abstract
This chapter mainly discusses the flow details and characterization performance of gas–gas fluidic throat, including the effective throat area of fluidic throat, the analytical methods for steady aerodynamic characteristics, flow characteristics of fluidic, relationship between secondary flow rate ratio and total pressure ratio, relationship between secondary flow parameters and effective throat area, effect of the main nozzle parameters, and comparison of secondary flow injection schemes in the fluidic throat.
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References
Miller, D.N., Catt, J.A.: Conceptual development of fixed-geometry nozzles using fluidic injection for throat-area control. AIAA-95-2603
McArdle, J.G.: Internal characteristics and performance of an aerodynamically controlled, variable discharge convergent nozzle. NACA-TN4312, July 1958
Damiel, Y., Miller, N., Patrick, J.Y., Jeffrey, W.H.: Fluidic throat skewing for thrust vectoring in fixed-geometry nozzles. AIAA-99-0365
Baruzzini, D., Domel, N., Miller, D.N., et al.: Pulsed injection flow control for throttling in supersonic nozzles—a computational fluid dynamics design study. AIAA-2007-4215
Xie, K.: Numerical and Experimental Study on Fluid Throat of Solid Rocket Engine. Beihang University, Beijing
Kan, X., Yu, L., Wang, Y.B.: Steady numerical study of aerodynamic throat formed by round injectors. J. Aerosp. Power 26(4), 924–930 (2011)
Wang, Y.L., Guo-Qiang, H.E., Jiang, L.I., et al.: Experiment on non-coaxial variable thrust pintle solid motor. J. Solid Rocket Technol. (2008)
Juan, L.I., Jiang, L.I., Wang, Y.L., et al.: Study on performance of pintle controlled thrust solid rocket motor. J. Solid Rocket Technol. 30(6), 505–509 (2007)
Wang, F.: Computational Fluid Dynamics Analysis. Tsinghua University Press, Beijing (2004)
Tao, W.: Computational Fluid Dynamics and Heat Transfer. China Architecture & Building Press, Beijing (1991)
Zheng, Ya., Chen, J., et al.: Solid Rocket Motor Heat Transfer. Beihang University Press, Beijing (2006)
Ma, T.: Computational Fluid Dynamics. Beijing Aviation Academy Press, Beijing (1986)
Yan, C.: Computational Fluid Dynamics Method and Application. Beihang University Press, Beijing (2006)
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© 2019 Springer Nature Singapore Pte Ltd. and National Defense Industry Press
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Xie, K., Chen, X., Li, J., Liu, Y. (2019). Steady Characteristics of a Gas–Gas Aerodynamic Throat. In: Fluidic Nozzle Throats in Solid Rocket Motors. Springer, Singapore. https://doi.org/10.1007/978-981-13-6439-6_2
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DOI: https://doi.org/10.1007/978-981-13-6439-6_2
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