Devising a method to design supersonic nozzles of rocket engines by using numerical analysis methods
, 2023 Ivan Dubrovskiy, Valeriy Bucharskyi
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Results in EngineeringThe rotating detonation engine (RDE) is an innovative pressure-gain combustion device that harnesses detonation waves for efficient fuel combustion.
Guining Liu +6 more
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Comparison of two procedures for predicting rocket engine nozzle performance [PDF]
23rd Joint Propulsion Conference, 1987 Two nozzle performance prediction procedures which are based on the standardized JANNAF methodology are presented and compared for four rocket engine nozzles. The first procedure required operator intercedence to transfer data between the individual performance programs.
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DESIGN AND ANALYSIS OF AEROSPIKE BELL NOZZLE TO IMPROVE THRUST IN ROCKET ENGINE
, 2022 A J Sriganapathy +2 more
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A Study on the Regenerative-Cooling Nozzle with Liquid Oxygen for Hybrid Rocket Engine - Part 1
, 2023 Young Il Park +6 more
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THERMO-STRENGTH ANALYSIS OF UNCOOLED COMPOSITE NOZZLE OF A LIQUID ROCKET ENGINE
, 2022 М. M. Dron’, K. I. Zharikov
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Numerical Investigation on the Effect of Fuel-Rich Degree in the RBCC Engine under the Ejector Mode
International Journal of Aerospace EngineeringThe ejector mode of the Rocket-Based Combined-Cycle (RBCC) engine is characterized by high fuel consumption. This study is aimed at investigating the influence of the rocket fuel-rich degree on the RBCC engine’s performance under the ejector mode ...
Yizhi Yao +9 more
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Cooling process of liquid propellant rocket by means of kerosene-alumina nanofluid
Propulsion and Power Research, 2016 Heat transfer augmentation of kerosene-alumina nanofluid is studied for the possible use in the regenerative cooling channel of semi cryogenic engine.
Mostafa Mahmoodi, Sh. Kandelousi
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Numerical Analysis of Convergent-Divergent Angles and Operating Conditions Impact on Rocket Nozzle Performance Parameters [PDF]
INCAS BulletinComprehensive numerical analysis was conducted to elucidate the exhaust performance of rocket engine nozzles. The study focused on unravelling the intricate relationship between convergence and divergence angles and their impact on the exhaust ...
Nabila ALILI +3 more
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Rocket engine design and optimization: Nozzle configuration and computational simulation
Buscà i Pahissa, Roger
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