Nonlinear theory of combustion stability in liquid rocket engine based on chemistry dynamics

Yuhui Huang; Zhenguo Wang; Jin Zhou

doi:10.1007/bf02879348

Nonlinear theory of combustion stability in liquid rocket engine based on chemistry dynamics

Science in China Series B Chemistry ◽

10.1007/bf02879348 ◽

2002 ◽

Vol 45 (4) ◽

pp. 373-383 ◽

Cited By ~ 6

Author(s):

Yuhui Huang ◽

Zhenguo Wang ◽

Jin Zhou

Keyword(s):

Nonlinear Theory ◽

Rocket Engine ◽

Combustion Stability ◽

Liquid Rocket Engine ◽

Liquid Rocket ◽

Chemistry Dynamics

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Nonlinear theory of combustion stability in liquid rocket engine based on chemistry dynamics

Science in China Series B Chemistry ◽

10.1360/02yb9047 ◽

2002 ◽

Vol 45 (4) ◽

pp. 373

Author(s):

Yuhui HUANG

Keyword(s):

Nonlinear Theory ◽

Rocket Engine ◽

Combustion Stability ◽

Liquid Rocket Engine ◽

Liquid Rocket ◽

Chemistry Dynamics

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Numerical simulation of combustion stability of liquid rocket engine based on chemistry dynamics

Science in China Series B Chemistry ◽

10.1360/02yb9072 ◽

2002 ◽

Vol 45 (5) ◽

pp. 551 ◽

Cited By ~ 3

Author(s):

Yuhui HUANG

Keyword(s):

Numerical Simulation ◽

Rocket Engine ◽

Combustion Stability ◽

Liquid Rocket Engine ◽

Liquid Rocket ◽

Chemistry Dynamics

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Design and Verification Test of Multiple-Injector Head Arranged in a Row for Combustion Stability Rating Test of a Liquid Rocket Engine

Transactions of the Korean Society of Mechanical Engineers B ◽

10.3795/ksme-b.2021.45.7.365 ◽

2021 ◽

Vol 45 (7) ◽

pp. 365-376

Author(s):

Seok Won Kim ◽

Jeong Hwa Oh ◽

Min Kyu Shin ◽

Do Hwan Gu ◽

Young Sung Ko

Keyword(s):

Rocket Engine ◽

Combustion Stability ◽

Liquid Rocket Engine ◽

Verification Test ◽

Stability Rating ◽

Liquid Rocket

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Effects of Finite-Rate Chemistry and Film Cooling on Linear Combustion-Stability Limit in Liquid Rocket Engine

Journal of the Korean Society for Aeronautical & Space Sciences ◽

10.5139/jksas.2006.34.2.075 ◽

2006 ◽

Vol 34 (2) ◽

pp. 75-81

Keyword(s):

Film Cooling ◽

Rocket Engine ◽

Stability Limit ◽

Combustion Stability ◽

Liquid Rocket Engine ◽

Finite Rate ◽

Liquid Rocket

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Global Model of Liquid Rocket Engine Combustion Instability Based on Chemistry Dynamics

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit ◽

10.2514/6.2002-3992 ◽

2002 ◽

Author(s):

Huang Yuhui ◽

Wang Zhenguo

Keyword(s):

Rocket Engine ◽

Combustion Instability ◽

Global Model ◽

Liquid Rocket Engine ◽

Engine Combustion ◽

Liquid Rocket ◽

Chemistry Dynamics

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Effect of Combined Hub/Blade Baffles on the Combustion Stability of a Liquid Rocket Engine

46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit ◽

10.2514/6.2010-6803 ◽

2010 ◽

Author(s):

Allan Kirkpatrick ◽

Tim Hinerman

Keyword(s):

Rocket Engine ◽

Combustion Stability ◽

Liquid Rocket Engine ◽

Liquid Rocket

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Combustion Stability Rating Test of Liquid Rocket Engine Thrust Chamber

Journal of the Korean Society of Propulsion Engineers ◽

10.6108/kspe.2014.18.2.060 ◽

2014 ◽

Vol 18 (2) ◽

pp. 60-66

Author(s):

Kyubok Ahn ◽

Jong-Gyu Kim ◽

Hwan-Seok Choi

Keyword(s):

Rocket Engine ◽

Combustion Stability ◽

Liquid Rocket Engine ◽

Thrust Chamber ◽

Engine Thrust ◽

Stability Rating ◽

Liquid Rocket

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The advanced liquid rocket engine line of SDO “Yuzhnoye” for the creation of new families of launch vehicles

Kosmìčna nauka ì tehnologìâ ◽

10.15407/knit2015.05.028 ◽

2015 ◽

Vol 21 (5(96)) ◽

pp. 28-35

Author(s):

А.А. Prokopchuk ◽

◽

V.А. Shulga ◽

Keyword(s):

Rocket Engine ◽

Liquid Rocket Engine ◽

Launch Vehicles ◽

The Creation ◽

Liquid Rocket

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NUMERICAL SIMULATIONS ON THE COOLING JACKET CHANNEL OF A REGENERATIVELY COOLED LIQUID ROCKET ENGINE

Proceeding of Proceedings of CHT-17 ICHMT International Symposium on Advances in Computational Heat Transfer May 28-June 1, 2017, Napoli, Italy ◽

10.1615/ichmt.2017.330 ◽

2017 ◽

Author(s):

Daniele Ricci ◽

Francesco Battista ◽

Pasquale Natale ◽

Manrico Fragiacomo

Keyword(s):

Numerical Simulations ◽

Rocket Engine ◽

Liquid Rocket Engine ◽

Cooling Jacket ◽

Liquid Rocket

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Mechanical Disturbances Arising From Thermal Power Deposition in a Gas with Application to Supercritical Liquid Rocket Engine Combustion Instability

51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition ◽

10.2514/6.2013-567 ◽

2013 ◽

Cited By ~ 1

Author(s):

David Kassoy

Keyword(s):

Rocket Engine ◽

Thermal Power ◽

Combustion Instability ◽

Liquid Rocket Engine ◽

Power Deposition ◽

Engine Combustion ◽

Liquid Rocket ◽

Mechanical Disturbances

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