LEADER 01867nam  2200469I  450 
001 9910707944203321
005 20170207133449.0
035   $a(CKB)5470000002469127
035   $a(OCoLC)971548660
035   $a(EXLCZ)995470000002469127
100   $a20170207j201609    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aIce-accretion test results for three large-scale swept-wing models in the NASA Icing Research Tunnel /$fAndy P. Broeren [and five others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dSeptember 2016.
215   $a1 online resource (34 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2016-219137
300   $a"September 2016."
300   $a"Prepared for the 8th Atmospheric and Space Environments Conference sponsored by the American Institute of Aeronautics and Astronautics, Washington D.C., June 13-17, 2016."
300   $a"AIAA-2016-3733."
320   $aIncludes bibliographical references (pages 32-34).
606   $aAerodynamic characteristics$2nasat
606   $aAircraft icing$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aComputerized simulation$2nasat
606   $aThree dimensional models$2nasat
615  7$aAerodynamic characteristics.
615  7$aAircraft icing.
615  7$aComputational fluid dynamics.
615  7$aComputerized simulation.
615  7$aThree dimensional models.
700   $aBroeren$b Andy P.$01386216
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707944203321
996   $aIce-accretion test results for three large-scale swept-wing models in the NASA Icing Research Tunnel$93532254
997   $aUNINA