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035   $a(OCoLC)858259381
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100   $a20130912j199810    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aImpingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel /$fRichard J. Re and Francis J. Capone
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dOctober 1998.
215   $a1 online resource (37 pages) $cillustrations
225 1 $aNASA/TM ;$v1998-208723
300   $a"October 1998."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 7).
606   $aSupersonic transports$2nasat
606   $aSupersonic speed$2nasat
606   $aStatic pressure$2nasat
606   $aShock waves$2nasat
606   $aMach number$2nasat
606   $aBow waves$2nasat
606   $aBodies of revolution$2nasat
615  7$aSupersonic transports.
615  7$aSupersonic speed.
615  7$aStatic pressure.
615  7$aShock waves.
615  7$aMach number.
615  7$aBow waves.
615  7$aBodies of revolution.
700   $aRe$b Richard J.$01387323
702   $aCapone$b Francis J.
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910705811003321
996   $aImpingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel$93437009
997   $aUNINA