50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2012
DOI: 10.2514/6.2012-582
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Effect of Boundary Layer on Choked Flow through a Rectangular Convergent Nozzle

Abstract: The experimentaI results 〔 }f the ch 〔, king pressure ratio and the choked 日ow rate in u c nverging nezzle are con / pared with three theoretical values calculated by the Fanno 且 w theory , the compound fioLv mode1 , and thc average now rn 〔 〕deL The experiment . atvalues are in qualita 亡 ive agreenler ユt with the calculated va ] ues in any of these cases , and agree best with the 、 ・ alucs by し he average 飾 w m σde1 . Based upon thcse compar 孟 sons , the mechanism of the choking of the flow where し he velocit… Show more

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