LEADER 01993nam  2200529I  450 
001 9910707178503321
005 20160420133300.0
035   $a(CKB)5470000002461710
035   $a(OCoLC)946998844
035   $a(EXLCZ)995470000002461710
100   $a20160420j199608    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMinimum weight design of a generic axisymmetric inlet /$fShari-Beth Nadell
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dAugust 1996.
215   $a1 online resource (13 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107288
300   $aTitle from title screen (viewed April 20, 2016).
300   $a"Prepared for the 32nd Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Lake Buena Vista, Florida, July 1-3, 1996."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 9).
606   $aSymmetry$2nasat
606   $aAir intakes$2nasat
606   $aFinite element method$2nasat
606   $aSupersonic inlets$2nasat
606   $aStructural design$2nasat
606   $aStructural weight$2nasat
606   $aEngine design$2nasat
615  7$aSymmetry.
615  7$aAir intakes.
615  7$aFinite element method.
615  7$aSupersonic inlets.
615  7$aStructural design.
615  7$aStructural weight.
615  7$aEngine design.
700   $aNadell$b Shari-Beth$01411929
712 02$aLewis Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707178503321
996   $aMinimum weight design of a generic axisymmetric inlet$93504167
997   $aUNINA