Kenneth John Kacynski

• A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis
• A three-dimensional turbulent heat transfer analysis for advanced tubular rocket thrust chambers
• Calculation of propulsive nozzle flowfields in multidiffusing chemically recating environments
• Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle
• The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios
• Thermal stratification potential in rocket engine coolant channels