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Transient induced delay in the check injector of the ADDA combined rocket motor

机译：aDDa组合火箭发动机的止回喷射器中的瞬态诱导延迟

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Rugescu Radu D; Calcisca Gabriel; Rugescu Ronald D;
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1. A LINEAR STABILITY ANALYSIS OF OSCILLATORY COMBUSTION INDUCED BY COMBUSTION TIME DELAYS OF LIQUID OXIDIZER IN HYBRID ROCKET MOTORS [J] . Takakazu Morita, Koki Kitagawa, Toru Shimada, International journal of energetic materials and chemical propulsion . 2014,第1期

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2. Flow field and injector heat characteristics of hybrid rocket motor with annular-gap injector [J] . Li Chengen, Cai Guobiao, Wang Pengfei, Aerospace science and technology . 2019,第Octa期

机译：带环形间隙喷射器的混合火箭发动机的流场和喷射器热特性
3. Robust stabilization of input-delayed systems with design example for rocket motor control [J] . Elbrous M. Jafarov Aircraft Engineering and Aerospace Technology . 2008,第1期

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4. Transient induced delay in the check injector of the ADDA combined rocket motor [C] . RUGESCU Radu D., CALCISCA Gabriel, RUGESCU Ronald D. IEEE/IACSIT/SCIEI International Conference on Aerospace, Robotics, Mechanical Engineering, Manufacturing Systems, Biomechanics, Neurorehabilitation and Human Motricities . 2013

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5. Numerical Modelling of Staged Combustion Aft-Injected Hybrid Rocket Motors. [D] . Nijsse, Jeff. 2012

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6. Acute transient hemorrhagic hypotension does not aggravate structural damage or neurologic motor deficits but delays the long-term cognitive recovery following mild to moderate traumatic brain injury [O] . Christian Schütz, John F. Stover, Hilaire J. Thompson, -1

机译：急性短暂性出血性低血压不会加重结构损伤或神经运动功能障碍但会延迟轻度至中度外伤性脑损伤后的长期认知恢复
7. Coupling of Level Set and Volume of Fluid Methods for Simulations of Transient Internal Flow Field in Solid Rocket Motors [O] . Ze Zhang, Feng Gao, Rui Lv, 2021

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8. An experimental correlation of the nonreactive properties of injection schemes and combustion effects in a liquid-propellant rocket engine. part 1- the application of nonreactive-spray properties to rocket-motor injector design [R] . Rupe, J. H. 1965

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Transient induced delay in the check injector of the ADDA combined rocket motor

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