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NASA-TM-76710

Influence of the Reynolds number on the normal forces of slender bodies of revolution

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:57:05Z
date available2017-09-04T15:57:05Z
date copyright01/01/1982
date issued1982
identifier otherQZMKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/60408
description abstractComprehensive force, moment, and pressure distribution measurements as well as flow visualization experiments were carried out to determine the influence of the Reynolds number on nonlinear normal forces of slender bodies of revolution. Experiments were performed in transonic wind tunnels at angles of attack up to 90 deg in the Mach number range 0.5 to 2.2 at variable Reynolds numbers. The results were analysed theoretically and an empirical theory was developed which describes the test results satisfactory.
languageEnglish
titleNASA-TM-76710num
titleInfluence of the Reynolds number on the normal forces of slender bodies of revolutionen
typestandard
page31
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1982
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsANGLE
subject keywordsATTACK
subject keywordsBODIES
subject keywordsBOUNDARY
subject keywordsDISTRIBUTION
subject keywordsFLOW
subject keywordsFORCE
subject keywordsFORCES
subject keywordsLAYER
subject keywordsMOMENT
subject keywordsNUMBER
subject keywordsPRESSURE
subject keywordsREVOLUTION
subject keywordsREYNOLDS
subject keywordsSEPARATION
subject keywordsSLENDER
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsVISUALIZATION
subject keywordsVORTICES
subject keywordsWIND


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