LEADER 01790nam  2200493I  450 
001 9910707928203321
005 20170525133947.0
035   $a(CKB)5470000002469289
035   $a(OCoLC)972501458
035   $a(EXLCZ)995470000002469289
100   $a20170214j201611    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena /$fMichael A. Kegerise and Dan H. Neuhart
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dNovember 2016.
215   $a1 online resource (118 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2016-219348
300   $a"November 2016."
300   $a"Performing organization: NASA Langley Research Center" Report documentation page.
320   $aIncludes bibliographical references (pages 30-31).
606   $aBody-wing configurations$2nasat
606   $aFlow distribution$2nasat
606   $aLaser doppler velocimeters$2nasat
606   $aReynolds number$2nasat
606   $aSubsonic wind tunnels$2nasat
606   $aWind tunnel models$2nasat
615  7$aBody-wing configurations.
615  7$aFlow distribution.
615  7$aLaser doppler velocimeters.
615  7$aReynolds number.
615  7$aSubsonic wind tunnels.
615  7$aWind tunnel models.
700   $aKegerise$b Michael A.$01397448
702   $aNeuhart$b Dan H$g(Dan Howard),$f1952-
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707928203321
996   $aWind tunnel test of a risk-reduction wing$93503867
997   $aUNINA