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100   $a20120408j196903    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMeasured effects of gaseous flow system dynamics on acoustic-mode combustion instability /$fby John F. Groenweg
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dMarch 1969.
215   $a1 online resource (ii, 15 pages) $cillustrations
225 1 $aNASA technical note ;$vNASA TN D-5080
300   $a"March 1969."
320   $aIncludes bibliographical references (page 15).
606   $aRocket engines$xCombustion
606   $aHydrogen as fuel
606   $aGas flow
606   $aGas dynamics
606   $aGas dynamics$2fast
606   $aGas flow$2fast
606   $aHydrogen as fuel$2fast
606   $aRocket engines$xCombustion$2fast
615  0$aRocket engines$xCombustion.
615  0$aHydrogen as fuel.
615  0$aGas flow.
615  0$aGas dynamics.
615  7$aGas dynamics.
615  7$aGas flow.
615  7$aHydrogen as fuel.
615  7$aRocket engines$xCombustion.
700   $aGroeneweg$b John F$g(John Frederick),$f1937-$01407187
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLewis Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bABC
801  2$bAD#
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bCOP
801  2$bGPO
906   $aBOOK
912   $a9910714097603321
996   $aMeasured effects of gaseous flow system dynamics on acoustic-mode combustion instability$93487865
997   $aUNINA