LEADER 01697nam  2200457I  450 
001 9910709683803321
005 20180522133832.0
035   $a(CKB)5470000002471395
035   $a(OCoLC)1037018754
035   $a(EXLCZ)995470000002471395
100   $a20180522j198309    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComputation of potential flows with embedded vortex rings and applications to helicopter rotor wakes /$fThomas W. Roberts
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration,$dSeptember 1983.
215   $a1 online resource (98 pages) $cillustrations
225 1 $aNASA/CR ;$v166542
300   $a"September 1983."
320   $aIncludes bibliographical references (pages 51-52).
606   $aPotential flow$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aComputational grids$2nasat
606   $aRotary wings$2nasat
606   $aFinite difference theory$2nasat
615  7$aPotential flow.
615  7$aComputational fluid dynamics.
615  7$aComputational grids.
615  7$aRotary wings.
615  7$aFinite difference theory.
700   $aRoberts$b Thomas W.$01412257
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aMassachusetts Institute of Technology.$bDepartment of Aeronautics and Astronautics.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910709683803321
996   $aComputation of potential flows with embedded vortex rings and applications to helicopter rotor wakes$93505239
997   $aUNINA