Numerical investigation on critical heat flux and coolant volume required for transpiration cooling with phase change
Author:
Publisher
Elsevier BV
Subject
Energy Engineering and Power Technology,Fuel Technology,Nuclear Energy and Engineering,Renewable Energy, Sustainability and the Environment
Reference23 articles.
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4. Landis JA. Numerical study of a transpiration cooled rocket nozzle. In: 32nd AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, July 1–3, Lake Buena Vista, FL; 1996. p. 1996–2580.
5. Effect of nozzle geometry on pressure drop and heat transfer in submerged jet arrays;Royne;Int J Heat Mass Trans,2006
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