Zhuang Fengchen, male, Han nationality, is a native of Changzhou, Jiangsu Province. He graduated from the Harbin Polytechnics University in 1956.
Zhuang Fengchen initiated the high-pressure evaporation model of liquid propellants and conducted research on the non-ideality of high-pressure phase balances and liquid mechanics properties, non-stationary of gas and liquid boundary surface movement and process, and the decomposition and dissociation reaction of propellants.
Zhuang studied the hypergolic propellant rocket engine combustion process calculation comprehensive model and changed the regulation of the combustion performance of the engine. He then researched the value appraisal technology of MMH/NTO rocket engine combustion acoustics instability and sound cavity damps. He also researched the atomization mechanism and combustion property of oxyhydrogen engine injectors and established the atomization property calculation model and atomizing combustion model.
Zhuang was elected an academician of the Chinese Academy of Sciences in 2001.
2001— | Academician, Chinese Academy of Sciences | |
Professor, (Outfit Command Technology Institute) | ||
1956 | Graduate, Harbin Polytechnics University, Power Machinery Department Heilongjiang Province, Harbin City |