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035   $a(OCoLC)785925432
035   $a(EXLCZ)995470000002419712
100   $a20120417d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComputational analysis of a low-boom supersonic inlet$b[electronic resource] /$fRodrick V. Chima
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2011]
215   $a1 online resource (14 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2011-217223
300   $aTitle from title screen (viewed on Apr. 17, 2012).
300   $a"November 2011."
300   $a"Prepared for the 29th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics, Honolulu, Hawaii, June 27-30, 2011."
300   $a"AIAA-2011-3801."
320   $aIncludes bibliographical references (pages 13-14).
606   $aComputational fluid dynamics$2nasat
606   $aEngine inlets$2nasat
606   $aSupersonic aircraft$2nasat
606   $aSupersonic inlets$2nasat
606   $aInlet airframe configurations$2nasat
606   $aOverpressure$2nasat
606   $aSupersonic flow$2nasat
606   $aSonic booms$2nasat
606   $aWind tunnel tests$2nasat
615  7$aComputational fluid dynamics.
615  7$aEngine inlets.
615  7$aSupersonic aircraft.
615  7$aSupersonic inlets.
615  7$aInlet airframe configurations.
615  7$aOverpressure.
615  7$aSupersonic flow.
615  7$aSonic booms.
615  7$aWind tunnel tests.
700   $aChima$b Rodrick V$01393796
712 02$aNASA Glenn Research Center.
712 12$aAIAA Applied Aerodynamics Conference$d(29th :$f2011 :$eHonolulu, Hawaii)
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910701537703321
996   $aComputational analysis of a low-boom supersonic inlet$93523558
997   $aUNINA