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001 9910706187803321
005 20170818131353.0
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035   $a(OCoLC)844618356
035   $a(EXLCZ)995470000002454546
100   $a20130526j199907    uh             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDesign and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment /$fDonald Greer [and three others]
210  1$aEdwards, California :$cNational Aeronautics and Space Administration, Dryden Flight Research Facility,$dJuly 1999.
215   $a1 online resource (17 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-206579
300   $a"July 1999."
300   $a"Presented at the 17th Applied Aerodynamics Conference and 14th Computational Fluid Dynamics Conference, Norfolk, Virginia, June 28-July 1, 1999, AIAA 99-3183"--Report documentation page.
300   $a"Performing organization: NASA Dryden Flight Research Center and Technische Universita?t Mu?nchen"--Report documentation page.
320   $aIncludes bibliographical references (pages 16-17).
517   $aDesign and predictions for a high-altitude 
606   $aAirfoils$2nasat
606   $aHigh altitude$2nasat
606   $aLow Reynolds number$2nasat
606   $aNavier-Stokes equation$2nasat
606   $aAerodynamic drag$2nasat
606   $aStatic pressure$2nasat
606   $aSubsonic speed$2nasat
606   $aBoundary layer stability$2nasat
606   $aFlight tests$2nasat
615  7$aAirfoils.
615  7$aHigh altitude.
615  7$aLow Reynolds number.
615  7$aNavier-Stokes equation.
615  7$aAerodynamic drag.
615  7$aStatic pressure.
615  7$aSubsonic speed.
615  7$aBoundary layer stability.
615  7$aFlight tests.
700   $aGreer$b Donald$f1896-$01401785
712 02$aDryden Flight Research Facility,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910706187803321
996   $aDesign and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment$93470981
997   $aUNINA