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100   $a20111115j196903    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCharacteristics study of a bicone mixed-compression inlet for Mach 1.80 to 2.50 /$fby Bernhard H. Anderson
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dMarch 1969.
215   $a1 online resource (ii, 33 pages) $cillustrations
225 1 $aNASA technical note. ;$vTN D-5084
300   $a"March 1969."
320   $aIncludes bibliographical references (page 13).
606   $aAirplanes$xDesign and construction
606   $aJet engines$xAir intakes
606   $aAirplanes$xDesign and construction$2fast
606   $aJet engines$xAir intakes$2fast
615  0$aAirplanes$xDesign and construction.
615  0$aJet engines$xAir intakes.
615  7$aAirplanes$xDesign and construction.
615  7$aJet engines$xAir intakes.
700   $aAnderson$b Bernhard H.$01386038
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLewis Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bCOP
801  2$bGPO
906   $aBOOK
912   $a9910714098503321
996   $aCharacteristics study of a bicone mixed-compression inlet for Mach 1.80 to 2.50$93451462
997   $aUNINA