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NACA-TR-D-1374

The similarity rules for second-order subsonic and supersonic flow

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:48:13Z
date available2017-09-04T17:48:13Z
date copyright01/01/1958
date issued1958
identifier otherEQONEEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/171409
description abstractThe similarity rules for linearized compressible flow theory (Gothert's rule and its supersonic counterpart) are extended to second order. It is shown that any second-order subsonic flow can be related to "nearly incompressible" flow past the same body, which can be calculated by the Janzen-Rayleigh method.
languageEnglish
titleNACA-TR-D-1374num
titleThe similarity rules for second-order subsonic and supersonic flowen
typestandard
page8
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1958
contenttypefulltext
subject keywordsBODIES OF REVOLUTION
subject keywordsCOMPRESSIBLE FLOW
subject keywordsCONES
subject keywordsCYLINDRICAL BODIES
subject keywordsFLOW THEORY
subject keywordsSIMILITUDE LAW
subject keywordsSTEADY FLOW
subject keywordsSUBSONIC FLOW
subject keywordsSUPERSONIC FLOW
subject keywordsTHREE DIMENSIONAL BODIES


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