LEADER 01830nam  2200481   450 
001 9910707196803321
005 20160426151029.0
035   $a(CKB)5470000002461525
035   $a(OCoLC)947889608
035   $a(EXLCZ)995470000002461525
100   $a20160426j201512    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCalculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method /$fDonald R. Riley
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dDecember 2015.
215   $a1 online resource (61 pages) $cillustrations
225 1 $aNASA/TM ;$v2015-218998
300   $aTitle from title screen (viewed April 26, 2016).
300   $a"December 2015."
300   $a"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
320   $aIncludes bibliographical references (page 14).
606   $aAerodynamic coefficients$2nasat
606   $aAerodynamic stability$2nasat
606   $aAirfoils$2nasat
606   $aTime dependence$2nasat
606   $aVortices$2nasat
615  7$aAerodynamic coefficients.
615  7$aAerodynamic stability.
615  7$aAirfoils.
615  7$aTime dependence.
615  7$aVortices.
700   $aRiley$b Donald R.$01386410
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707196803321
996   $aCalculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method$93544733
997   $aUNINA