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NACA-TN-2744

Practical calculation of second-order supersonic flow past nonlifting bodies of revolution

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:10:01Z
date available2017-09-04T16:10:01Z
date copyright01/01/1952
date issued1952
identifier otherSILUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/73326
description abstractCalculation of second-order supersonic flow past bodies of revolution at zero angle of attack is described in detail, and reduced to routine computation. Use of an approximate tang-ency condition is shown to increase the accuracy for bodies with corners. Tables of basic functions and standard computing forms are presented. The procedure is summarized so that one can apply it without necessarily understanding the details of the theory. A sample calculation is given, and several examples are compared with solutions calculated by the method of characteristics.
languageEnglish
titleNACA-TN-2744num
titlePractical calculation of second-order supersonic flow past nonlifting bodies of revolutionen
typestandard
page68
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1952
contenttypefulltext
subject keywordsANALYSIS
subject keywordsANGLE
subject keywordsATTACK
subject keywordsBODIES
subject keywordsCHARACTERISTICS
subject keywordsCOMPARISON
subject keywordsCORNERS
subject keywordsDATA
subject keywordsDISTRIBUTION
subject keywordsFLOW
subject keywordsFUNCTIONS
subject keywordsMATHEMATICS
subject keywordsMETHOD
subject keywordsPREDICTION
subject keywordsPRESSURE
subject keywordsREVOLUTION
subject keywordsSUPERSONIC
subject keywordsTABLES
subject keywordsTECHNIQUES


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