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181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEstimation of aircraft nonlinear unsteady parameters from wind tunnel data /$fVladislav Klein, Patrick C. Murphy
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dDecember 1998.
215   $a1 online resource (38 pages) $cillustrations
225 1 $aNASA TM ;$v1998-208969
300   $a"December 1998."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 16-17).
606   $aWind tunnel tests$2nasat
606   $aUnsteady aerodynamics$2nasat
606   $aAerodynamic forces$2nasat
606   $aMathematical models$2nasat
606   $aAircraft stability$2nasat
606   $aFlight stability tests$2nasat
615  7$aWind tunnel tests.
615  7$aUnsteady aerodynamics.
615  7$aAerodynamic forces.
615  7$aMathematical models.
615  7$aAircraft stability.
615  7$aFlight stability tests.
700   $aKlein$b Vladislav$01385898
702   $aMurphy$b Patrick C.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910706191403321
996   $aEstimation of aircraft nonlinear unsteady parameters from wind tunnel data$93434331
997   $aUNINA