Heat Transfer of the Critical Air Flow In a Nozzle : 1st Report; Numerical Study on Heat Transfer of the Critical Air Flow in a Nozzle with Parallel Walls
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概要
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The heat transfer of a critical flow in a small-sized nozzle has not been studied in detail, since the flow is too complicated. In this paper, the two-dimensional compressible laminar boundary layer equations in a parallel nozzle with heat transfer are solved numerically. The obtained results reveal that the two-dimensional critical flow patterns are classified by "nozzle characteristic number x_c". The local and mean heat transfer coefficients in the critical nozzles were calculated by defining an adiabatic wall temperature as gas temperature in reference. Especially, it is found that the local heat transfer coefficients rise sharply near the nozzle exit. The mean Nusselt numbers obtained numerically can be plotted on a single curve independent of the non-dimensional wall temperature θ_w, being arranged on the basis of "modified nozzle characteristic Reynolds number X_<cdw>"; furthermore they can be approximated by incompressible ones, if arranged on the basis of "X_<cdws>^<-1>" defined as the state of sonic point in the critical nozzle.
- 一般社団法人日本機械学会の論文
著者
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Kashiwagi Takao
Department Of Mechanical Engineering For Production Tokyo Institute Of Technology
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Kurosaki Yasuo
Tokyo Institute Of Technology
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ISSHIKI Naotsugu
Tokyo Institute of Technology
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- Heat Transfer of the Critical Air Flow in a Nozzle : 3rd Report, Study on Heat Transfer of the Critical Air Flow in a Convergent Nozzle
- Heat Transfer of the Critical Air Flow In a Nozzle : 1st Report; Numerical Study on Heat Transfer of the Critical Air Flow in a Nozzle with Parallel Walls
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