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High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation [microform] / Robert S. Jankovsky and Timothy D. Smith, Albert J. Pavli (NASA/TP ; 1999-208522)

High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation [microform] / Robert S. Jankovsky and Timothy D. Smith, Albert J. Pavli (NASA/TP ; 1999-208522)
Microform図書
1999<YCA-NAS 1.60:208522>
National Diet Library
  • Subject HeadingBoundary layer thickness Rocket nozzles Combustion cha...

Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer [microform] / Abdelkader Frendi (NASA contractor report ; 201691)

Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer [microform] / Abdelkader Frendi (NASA contractor report ; 201691)
Microform図書
1997<YCA-NAS 1.26:201691>
National Diet Library
  • Subject Heading...boundary layer Boundary layer thickness High frequencies

Method of variational imbedding for identification of boundary-layer-thickness as an inverse problem

Method of variational imbedding for identification of boundary-layer-thickness as an inverse problem
Digital文書・図像類
Marinov, Tchavdar T., Christov, Christo I.航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.325-330
Other Libraries in Japan
  • Subject Heading... flow velocity boundary layer thickness boundary layer......rical analysis boundary layer thickness identification
  • Note (General)... and hence the boundary layer thickness is an artifici......ication of the boundary layer thickness. The original inverse problem...

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