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Evaluation of simultaneous effects of inlet stagnation pressure and heat transfer on condensing water-vapor flow in a supersonic Laval nozzle

机译：评价入口停滞压力和传热对超音速拉瓦尔喷嘴中冷凝水蒸气流的同时影响

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Amiri Rad E.; Mahpeykar M.R.; Teymourtash A.R.;
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1. Analytical investigation of simultaneous effects of convergent section heating of Laval nozzle, steam inlet condition, and nozzle geometry on condensation shock [J] . Somesaraee Makan Talebi, Rad Ehsan Amiri, Mahpeykar Mohammad Reza Journal of thermal analysis and calorimetry . 2018,第2期

机译：薰衣草喷嘴，蒸汽入口条件和喷嘴几何聚集段加热同时效应的分析研究凝结冲击
2. Effect of Slip Velocity and Heat Transfer on the Condensed Phase Momentum Flux of Supersonic Nozzle Flows [J] . S.A.Sherif, W.E.Lear, N.S.Winowich Journal of Fluids Engineering: Transactions of the ASME . 2000,第1期

机译：滑移速度和传热对超音速喷嘴流的凝结动量通量的影响
3. Reducing entropy generation by volumetric heat transfer in a supersonic two-phase steam flow in a Laval nozzle [J] . M.R. Mahpeykar, A.R. Teymourtash, E. Amiri Rad International Journal of Exergy . 2011,第1期

机译：降低拉瓦尔喷嘴超音速两相蒸汽流中体积传热引起的熵产生
4. Simultaneous Effects of Inlet Stagnation Pressure and Heat Transfer to the Water Vapor Condensing Flow of Supersonic Laval Nozzle [C] . E. Amiri Rad, M. R. Mahpeykar, A. R. Teymourtash International Meeting of Advances in Thermofluids . 2012

机译：入口停滞压力和热传递对超声波喷嘴水蒸气冷凝流的同步效果
5. Experimental pressure and heat transfer investigation over a "directed-energy air spike" inlet at flow mach numbers of 10 to 20, stagnation temperature of 1000 K, and arc powers up to 127 KW. [D] . Toro, Paulo Gilberto de Paula. 1998

机译：在流量为10至20的马赫数，停滞温度为1000 K，电弧功率高达127 KW的“定向能空气尖峰”入口上进行实验压力和传热研究。
6. Effects of two-phase inlet quality mass velocity flow orientation and heating perimeter on flow boiling in a rectangular channel: Part 1 – Two-phase flow and heat transfer results [O] . Chirag R. Kharangate, Lucas E. O’Neill, Issam Mudawar -1

机译：两相入口质量质量速度流向和加热周长对矩形通道中流沸腾的影响：第1部分–两相流和传热结果
7. Effects of Condensing Flow on an Oblique Shok Wave in a Supersonic Nozzle [O] . Soon Bum KWON, Kazuyasu MATSUO, Shigetoshi KAWAGOE, 1989

机译：冷凝流量对超声喷嘴倾斜冲击波的影响
8. Calculations of the Compressible Turbulent Boundary Layer with Pressure Gradient and Heat Transfer in Internal Flows with Particular Reference to Supersonic Nozzles [R] . E. R. BERGSTROM, S. RAGHUNATHAN 1971

机译：具有压力梯度和内部传热的可压缩湍流边界层的计算，特别参考超音速喷嘴

Evaluation of simultaneous effects of inlet stagnation pressure and heat transfer on condensing water-vapor flow in a supersonic Laval nozzle

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