A Comparative Study of Dual Throat Nozzles for Fluidic Thrust Vectoring Applications
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-97-1306-6_33
Reference10 articles.
1. Wu K, Kim HD (2021) A fluidic thrust vector control using the bypass flow in a dual throat nozzle. J Mech Sci Technol 35(08):3435–3443
2. Jain S, Roy S, Gupta D, Kumar V, Kumar N (2015) Study on fluidic thrust vectoring techniques for application in V/STOL aircrafts. In: SAE technical paper
3. Wu K, Kim TH, Kim HD (2021) Visualization and analysis on the thrust vectoring control in three-dimensional dual-throat nozzles. Visual Soc Jpn 24:891–915
4. Wang Y, Xu J, Huang S, Lin Y, Jiang J (2019) Computational study of axisymmetric divergent bypass dual throat nozzle. Int J Aerosp Sci Technol 86:177–190
5. Wang YS, Xu JL, Huang S (2017) Study of starting problem of axisymmetric divergent dual throat nozzle. J Eng Gas Turb Power 139(6):062602
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