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Keiichi Karashima



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An approximate approach to base flow behind two-dimensional rearward-facing steps placed in a uniform supersonic stream (Report / Institute of Space and Aeronautical Science, University of Tokyo)
Author: Keiichi Karashima
Manufacturer: Institute of Space and Aeronautical Science, University of Tokyo
 Instability of shock wave on thin airfoil in high subsonic flow (Aeronautical Research Institute report)
Author: Keiichi Karashima
Manufacturer: Aeronautical Research Institute, Univ. of Tokyo
 An integral analysis of heat transfer downstream of a rearward-facing step with small coolant injection (NASA technical note, NASA TN)
Author: Keiichi Karashima
Manufacturer: [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.]


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Keiichi Karashima


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