LEADER 01915nam  2200481   450 
001 9910705291903321
005 20141029154907.0
035   $a(CKB)5470000002448444
035   $a(OCoLC)889960525
035   $a(EXLCZ)995470000002448444
100   $a20140904j201307    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBackground pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel /$fRaymond Castner [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJuly 2013.
215   $a1 online resource (12 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2013-217903
300   $aTitle from title screen (viewed on Sept. 4, 2014).
300   $a"July 2013."
300   $a"Prepared for the 43rd Fluid Dynamics Conference and Exhibit sponsored by the American Institute of Aeronautics and Astronautics, San Diego, California, June 24-27, 2013."
320   $aIncludes bibliographical references (page 12).
606   $aPressure distribution$2nasat
606   $aSonic booms$2nasat
606   $aSpatial distribution$2nasat
606   $aSupersonic wind tunnels$2nasat
606   $aWind pressure$2nasat
615  7$aPressure distribution.
615  7$aSonic booms.
615  7$aSpatial distribution.
615  7$aSupersonic wind tunnels.
615  7$aWind pressure.
700   $aCastner$b Raymond S.$01392322
712 02$aNASA Glenn Research Center,
712 02$aFundamental Aeronautics Program (U.S.),
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705291903321
996   $aBackground pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel$93446864
997   $aUNINA