LEADER 01663nam  2200481   450 
001 9910702454603321
005 20130125074444.0
035   $a(CKB)5470000002427622
035   $a(OCoLC)825105403
035   $a(EXLCZ)995470000002427622
100   $a20130125d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aInvestigation of "6X" scramjet inlet configurations /$fStephen J. Alter
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$d2012.
215   $a1 online resource (94 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2012-217761
300   $aTitle from title screen (viewed on Jan. 25, 2013).
300   $a"September 2012."
320   $aIncludes bibliographical references (pages 92-94).
606   $aSupersonic combustion ramjet engines$2nasat
606   $aSupersonic combustion$2nasat
606   $aHypersonic speed$2nasat
606   $aEngine inlets$2nasat
606   $aAerodynamic configurations$2nasat
606   $aHypersonic inlets$2nasat
615  7$aSupersonic combustion ramjet engines.
615  7$aSupersonic combustion.
615  7$aHypersonic speed.
615  7$aEngine inlets.
615  7$aAerodynamic configurations.
615  7$aHypersonic inlets.
700   $aAlter$b Stephen J.$01394616
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702454603321
996   $aInvestigation of "6X" scramjet inlet configurations$93534984
997   $aUNINA