Optimal design and numerical analysis of the rapid precooler

Under the background of highly compact heat exchanger design core for the hypersonic aerospace precooled engine, a rapid precooler is designed and its performance is simulated under the high-altitude background. To this end, firstly, according to the known parameter range, a plate tube-fin rapid pre...

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Veröffentlicht in:	Thermophysics and aeromechanics 2019, Vol.26 (1), p.119-132
Hauptverfasser:	Liu, K.-X., Ai, C.-A., Wang, X.-R., Cai, X.-F., Wang, Y.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace engineering Aerospace engines Computer simulation Design Finite volume method Genetic algorithms Heat exchangers Heat transfer High altitude Numerical analysis Parameters Physics Physics and Astronomy Scale effect Thermodynamics
Online-Zugang:	Volltext
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