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Cited article:

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Acta Astronautica 194 514 (2022)

Unsteady Flow in a Dual-Bell Nozzle with Displacement of an Extendible Section from the Initial to Working Position

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Hybrid Double-Divergent Nozzle as a Novel Alternative for Future Rocket Engines

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Journal of Visualization 24 (4) 711 (2021)

Supersonic Dual Bell Axisymmetric Minimum Length Nozzle Conception for High Propulsion Thrust

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International Journal of Aeronautical and Space Sciences 20 (3) 673 (2019)

LOX/CH4 Hot-Flow Testing of Dual-Bell Nozzles with Rapid-Expansion Extension

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Parametric Study of Supersonic Film Cooling in Dual Bell Nozzle for an Experimental Air-Kerosene Engine

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Specific Impulse Gain for KSLV-II with Combination of Dual Bell Nozzle and Expansion-Deflection Nozzle

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Journal of the Korean Society of Propulsion Engineers 22 (1) 16 (2018)

Numerical Study on Transition Characteristics of Dual Bell Nozzle with Expansion Ratio Fixed

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Journal of the Korean Society of Propulsion Engineers 21 (3) 68 (2017)

Ariane 5 Performance Optimization Using Dual-Bell Nozzle Extension

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Journal of Spacecraft and Rockets 53 (4) 743 (2016)