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035   $a(CKB)5470000002517794
035   $a(OCoLC)785286647$z(OCoLC)56097996$z(OCoLC)761260280
035   $a(EXLCZ)995470000002517794
100   $a20120408j196812    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn estimate of the supersonic flow field about an axisymmetric body with an N wave pressure trace /$fby Roger W. Luidens
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1968.
215   $a1 online resource (ii, 25 pages) $cillustrations
225 1 $aNASA/TN ;$vD-4935
300   $a"December 1968."
320   $aIncludes bibliographical references (page 25).
606   $aSonic booms$2nasat
606   $aSupersonic flow$2nasat
606   $aSonic boom$2fast
615  7$aSonic booms.
615  7$aSupersonic flow.
615  7$aSonic boom.
700   $aLuidens$b Roger W.$01392705
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bEGM
801  2$bAD#
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716031303321
996   $aAn estimate of the supersonic flow field about an axisymmetric body with an N wave pressure trace$93447848
997   $aUNINA