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100   $a20130912j199908    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStatic performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control /$fScott C. Asbury and Craig A. Hunter
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dAugust 1999.
215   $a1 online resource (134 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-209513
300   $a"August 1999."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 19-20).
606   $aExhaust nozzles$2nasat
606   $aPorosity$2nasat
606   $aHole geometry (mechanics)$2nasat
606   $aCavities$2nasat
606   $aThrust vector control$2nasat
615  7$aExhaust nozzles.
615  7$aPorosity.
615  7$aHole geometry (mechanics)
615  7$aCavities.
615  7$aThrust vector control.
700   $aAsbury$b Scott C.$01397878
702   $aHunter$b Craig A$g(Craig Allen),
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910706145403321
996   $aStatic performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control$93549351
997   $aUNINA