境界層を考えた圧縮流体のノズル内流動 : 第3報先細および末広ノズルの理論計算とシュリーレン写真実験結果

概要

論文の詳細を見る
The theoretical calculations of compressible gas flow of nozzle accompanied by laminer or turbulent boundary layer at its wall, are extended to the case of convergent and divergent nozzles in this paper, using assumptions, equations and methods similar to those of the foregoing papers, which discussed the parallel walled straight simple nozzle only. And Schrielen photographic experiments of miscellaneous nozzles of conv. div. and parallel walls are done. By the results from above calculations and experiments, there exists supersonic main flow inside the nozzle end of parallel nozzle, and though, of convergent nozzle. And in divergent nozzle, there are some cases where the acoustic line is put away from throat into the divergent part.
一般社団法人日本機械学会の論文
1954-09-25