LEADER 01560nam  2200445I  450 
001 9910711533403321
005 20181114120143.0
035   $a(CKB)5470000002484719
035   $a(OCoLC)1065525464
035   $a(EXLCZ)995470000002484719
100   $a20181114j201810    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aUsing pressure sensitive paint to measure aerodynamic forces on a rotor blade in hover /$fAnthony Neal Watkins [and five others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dOctober 2018.
215   $a1 online resource (52 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2018-220093
300   $a"October 2018."
320   $aIncludes bibliographical references (pages 23-26).
606   $aAerodynamic forces$2nasat
606   $aRotary wing aircraft$2nasat
606   $aHovering$2nasat
606   $aSubsonic wind tunnels$2nasat
606   $aWind tunnel tests$2nasat
615  7$aAerodynamic forces.
615  7$aRotary wing aircraft.
615  7$aHovering.
615  7$aSubsonic wind tunnels.
615  7$aWind tunnel tests.
700   $aWatkins$b Anthony Neal$01407931
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910711533403321
996   $aUsing pressure sensitive paint to measure aerodynamic forces on a rotor blade in hover$93519457
997   $aUNINA