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NUMERICAL AND EXPERIMENTAL STUDY OF SWIRL ATOMIZERS FOR LIQUID PROPELLANT ROCKET ENGINES

机译：液体推进剂火箭发动机旋流雾化器的数值和实验研究

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Brunno B. Vasques; Marcio Teixeira De Mendonça; Wladimyr Mattos; Costa Dourado;
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年度 2011
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1. EXPERIMENTAL INVESTIGATION OF CHARACTERISTICS OF A DOUBLE-BASE SWIRL INJECTOR IN A LIQUID ROCKET PROPELLANT ENGINE [J] . Fathollah OMMI, Koros NEKOFAR, Amir KARGAR, Thermal science . 2010,第2期

机译：液体火箭发动机双基旋流喷枪特性的实验研究
2. Experimental investigation of characteristics of a double-base swirl injector in a liquid rocket propellant engine [J] . Ommi Fathollah, Nekofar Koros, Kargar Amir, Thermal science . 2010,第2期

机译：液体火箭发动机双基涡旋喷油器特性的实验研究
3. Designing and Experimental Investigation of Characteristics of a Double-Base Swirl Injector in a Liquid Rocket Propellant Engine [J] . Fathollah Ommi, Kouros Nekofar, Ehsan Movahednejad Journal of applied sciences research . 2009,第18期

机译：液体火箭发动机双基旋流喷油器特性的设计与实验研究
4. NUMERICAL AND EXPERIMENTAL STUDY OF SWIRL ATOMIZERS FOR LIQUID PROPELLANT ROCKET ENGINES [C] . Brunno B. Vasques, Marcio Teixeira de Mendonca, Wladimyr Mattos da Costa Dourado ASME international mechanical engineering congress and exposition;IMECE2011 . 2012

机译：液体推进剂火箭发动机旋流原子器的数值和实验研究
5. Primary atomization study of a swirl coaxial liquid propellant rocket injector. [D] . Rahman, Shamim Aejaz. 1997

机译：涡旋同轴液体推进剂火箭喷射器的初步雾化研究。
6. Dataset of the experimentally measured heat transfer in the throat region of liquid rocket engine thrust chambers [O] . Marco Pizzarelli 2021

机译：实验测量的热传递的数据集在液体火箭发动机推力室的喉部区域中的热传递
7. Erratum to: “Numerical and experimental investigations of the effect of repeated cyclic thermal loads on the strength of materials of recoverable liquid-propellant rocket engines” [O] . V. I. Bubnov, D. V. Isakov, I. G. Lozino-Lozinskaya, 2009

机译：误解：“对重复循环热负荷对可回收液 - 推进式火箭发动机材料强度的数值和实验研究”
8. Modeling Liquid Rocket Engine Atomization and Swirl/Coaxial Injectors [R] . Heister, S. 2008

机译：液体火箭发动机雾化和旋流/同轴注射器的建模

NUMERICAL AND EXPERIMENTAL STUDY OF SWIRL ATOMIZERS FOR LIQUID PROPELLANT ROCKET ENGINES

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