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Applications of variable property heat- transfer and friction equations to rocket nozzle coolant passages and comparison with nuclear rocket test results

机译：可变性质的传热和摩擦方程在火箭喷嘴冷却剂通道中的应用以及与核火箭试验结果的比较

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Variable property heat transfer and friction equations to rocket nozzle coolant passages and comparison with nuclear rocket test results

机译：火箭喷嘴冷却剂通道的可变性质的传热和摩擦方程，并与核火箭测试结果进行比较

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Taylor M. F.;
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年度 1970
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1. WC-Co Coatings for High Temperature Rocket Nozzle Applications: An Applications Note [J] . Bondan T. Sofyan, Christopher C. Berndt, Marizki Stefano, International Journal of Technology . 2010 ,第1期

机译：用于高温火箭喷嘴应用的WC-Co涂层：应用说明
2. COMPUTATIONAL STUDY OF HEAT TRANSFER CHARACTERISTICS OF SUPERCRITICAL METHANE FLOW IN THE COOLANT CHANNEL OF A ROCKET ENGINE [J] . Mathew Saxon Arakkaparambil, Pradeep Kumar, Aravind Vaidyanathan High Temperature Material Processes . 2018 ,第2a3期

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3. LONG-RUN TESTING OF MODEL NOZZLE EXTENSIONS MADE OF A CARBON-CARBON COMPOSITE MATERIAL IN A LIQUID-PROPELLANT ROCKET ENGINE OPERATING ON HYDROGEN AND OXYGEN [J] . Anikin A. V., Berdov R. D., Volkov N. N., Journal of Applied Mechanics and Technical Physics . 2019 ,第1期

机译：在氢和氧作用下的液体火箭发动机中碳-碳复合材料制成的模型喷嘴延伸量的长期测试
4. NUCLEAR TESTING AND SAFETY COMPARISON OF NUCLEAR THERMAL ROCKET CONCEPTS [C] . David I. Poston Nuclear and emerging technologies for space topical meeting . 2018

机译：核热火箭概念的核试验和安全性比较
5. Nozzle erosion characterization and minimization for high-pressure rocket motor applications. [D] . Evans, Brian. 2010

机译：高压火箭发动机应用中的喷嘴腐蚀特性和最小化。
6. Quantitative Assessment of Amide Proton Transfer (APT) and Nuclear Overhauser Enhancement (NOE) Imaging with Extrapolated Semi-solid Magnetization Transfer Reference (EMR) Signals: II. Comparison of Three EMR Models and Application to Human Brain Glioma at 3 T [O] . Hye-Young Heo, Yi Zhang, Shanshan Jiang, -1

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7. Nuclear thermal rocket nozzle testing and evaluation program [O] . Davidian Kenneth O., Kacynski Kenneth J. 1993

机译：核热火箭喷嘴测试与评估程序
8. Applications of variable property heat- transfer and friction equations to rocket nozzle coolant passages and comparison with nuclear rocket test results [R] . Taylor, M. F. 1970

机译：可变特性传热和摩擦方程在火箭喷管冷却剂通道中的应用以及与核火箭试验结果的比较

Applications of variable property heat- transfer and friction equations to rocket nozzle coolant passages and comparison with nuclear rocket test results

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