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NACA-TR-1356

Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:09:09Z
date available2017-09-04T18:09:09Z
date copyright01/01/1958
date issued1958
identifier otherGTUYYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/192209
description abstractReport presents the results of experimental and theoretical research conducted on flow separation associated with steps, bases, compression corners, curved surfaces, shock-wave boundary-layer reflections, and configurations producing leading-edge separation. Results were obtained from pressure-distribution measurements, shadowgraph observations, high-speed motion pictures, and oil-film studies. The maximum scope of measurement encompassed Mach numbers between 0.4 and 3.6, and length Reynolds numbers between 4,000 and 5,000,000.
languageEnglish
titleNACA-TR-1356num
titleInvestigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transitionen
typestandard
page40
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1958
contenttypefulltext
subject keywordsBOUNDARY
subject keywordsCROCCO
subject keywordsDIMENSIONAL
subject keywordsFLAT
subject keywordsFLOW
subject keywordsLAMINAR
subject keywordsLAYER
subject keywordsLEE
subject keywordsMACH
subject keywordsNUMBER
subject keywordsPLATES
subject keywordsPOINTS
subject keywordsREATTACHED
subject keywordsREYNOLDS
subject keywordsSEPARATED
subject keywordsSEPARATION
subject keywordsSUBSONIC
subject keywordsSUPERSONIC
subject keywordsTESTS
subject keywordsTHEORY
subject keywordsTRANSITION
subject keywordsTUNNEL
subject keywordsTURBULENT
subject keywordsTWO
subject keywordsWIND


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