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An Experimental Investigation of Heat Transfer in the Nozzle of High-Aluminized Solid Rocket (Effects of Aluminum Added to Propellant)

机译：高铝固体火箭喷管传热实验研究（添加剂对铝的影响）

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作者
Godai, T.;
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作者单位

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年度 1969
页码 1-7
总页数 7
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aluminum ; Heat transfer coefficients ; Rocket nozzles ; Solid rocket propellants ; Gas flow ; Metal propellants ; Turbulent flow;

机译：铝;传热系数;火箭喷嘴;固体火箭推进剂;气流;金属推进剂;湍流;

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1. Features of heat transfer in a pre-nozzle volume of a solid-propellant rocket motor with charges of complex shapes [J] . B.Ya. Benderskiy, A.A. Chernova Thermophysics and Aeromechanics . 2018,第2期

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2. The effects of orifice nozzle number and nozzle made of polyamide plastic and aluminum with different inlet pressures on heating and cooling performance of counter flow Ranque-Hilsch vortex tubes: An experimental investigation [J] . Cebeci Ismail, Kirmaci Volkan, Topcuoglu Umit International Journal of Refrigeration . 2016,第Null期

机译：不同入口压力的节流孔喷嘴数量和聚酰胺塑料和铝制喷嘴对逆流Ranque-Hilsch涡流管加热和冷却性能的影响：实验研究
3. Numerical investigation of the influence of crystallization of ultrafine particles of aluminum oxide on energy characteristics of solid-propellant rocket engine [J] . Dyachenko N. N., Dyachenko L. I. Thermophysics and Aeromechanics . 2014,第4期

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4. The Role of Turbulent Oscillatory Flow on Investigation of Heat Transfer in Solid Propellant Rocket Motor [C] . M. Nasiri AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2002

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5. UNSTEADY FLAME ZONE COMBUSTION RESPONSE OF SOLID PROPELLANT ROCKET MOTORS (RADIATIVE HEAT TRANSFER, FUNCTION CALCULATIONS, PERTURBATION ANALYSES). [D] . KIM, PIL-KYU. 1985

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6. Dataset of the experimentally measured heat transfer in the throat region of liquid rocket engine thrust chambers [O] . Marco Pizzarelli 2021

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7. Investigation of Solid Propellant Rocket Motor Nozzle via CFD Simulation [O] . A. A. Al Mayas, Chen Aolin, Faieza Abdul Aziz, 2020

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8. A Comparison of Experimental Heat Transfer Coefficients in a Nozzle with Analytical Predictions from Bartz's Methods for Various Combustion Chamber Pressures in a Solid Propellant Rocket Motor [R] . Smith, D. M. 1970

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An Experimental Investigation of Heat Transfer in the Nozzle of High-Aluminized Solid Rocket (Effects of Aluminum Added to Propellant)

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