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NACA-TR-1135

Equations, tables, and charts for compressible flow

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:12:43Z
date available2017-09-04T15:12:43Z
date copyright01/01/1953
date issued1953
identifier otherLYDZYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/11266
description abstractThis report, which is a revision and extension of NACA-TN-1428, presents a compilation of equations, tables, and charts useful in the analysis of high-speed flow of a compressible fluid. The equations provide relations for continuous one-dimensional flow, normal and oblique shock waves, and Prandtl-Meyer expansions for both perfect and imperfect gases. The tables present useful dimensionless ratios for continuous one-dimensional flow and for normal shock waves as functions of Mach number for air considered as a perfect gas. One series of charts presents the characteristics of the flow of air (considered a perfect gas) for oblique shock waves and for cones in a supersonic air stream. A second series shows the effects of caloric imperfections on continuous one-dimensional flow and on the flow through normal and oblique shock waves. (author)
languageEnglish
titleNACA-TR-1135num
titleEquations, tables, and charts for compressible flowen
typestandard
page70
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1953
contenttypefulltext
subject keywordsAIR
subject keywordsCHARTS
subject keywordsCOMPRESSIBLE
subject keywordsDATA
subject keywordsDIMENSIONAL
subject keywordsEQUATIONS
subject keywordsEXPANSION
subject keywordsFLOW
subject keywordsGAS
subject keywordsGRAPHS
subject keywordsMACH
subject keywordsMEYER
subject keywordsNORMAL
subject keywordsNUMBER
subject keywordsOBLIQUE
subject keywordsONE
subject keywordsPRANDTL
subject keywordsRATIOS
subject keywordsSHOCK
subject keywordsSUBSONIC
subject keywordsSUPERSONIC
subject keywordsTABLES
subject keywordsWAVES


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