LEADER 01961nam  2200505I  450 
001 9910705754803321
005 20170621143343.0
035   $a(CKB)5470000002452859
035   $a(OCoLC)990345330
035   $a(EXLCZ)995470000002452859
100   $a20170621j199208    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLewis Icing Research Tunnel test of the aerodynamic effects of aircraft ground deicing/anti-icing fluids /$fL. James Runyan [and three others]
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dAugust 1992.
215   $a1 online resource (iii, 129 pages) $cillustrations
225 1 $aNASA technical paper ;$v3238
300   $a"August 1992"--Report documentation page.
300   $a"Performing organization: National Aeronautics and Space Administration Lewis Research Center"--Report documentation page.
606   $aAerodynamic characteristics$2nasat
606   $aBoeing aircraft$2nasat
606   $aDeicing$2nasat
606   $aIce formation$2nasat
606   $aNewtonian fluids$2nasat
606   $aRheology$2nasat
606   $aWind tunnel tests$2nasat
615  7$aAerodynamic characteristics.
615  7$aBoeing aircraft.
615  7$aDeicing.
615  7$aIce formation.
615  7$aNewtonian fluids.
615  7$aRheology.
615  7$aWind tunnel tests.
700   $aRunyan$b L. James$01411097
712 02$aLewis Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705754803321
996   $aLewis Icing Research Tunnel test of the aerodynamic effects of aircraft ground deicing$93501388
997   $aUNINA