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100   $a19910429j197212    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExtraction of longitudinal aerodynamic coefficients from forward-flight conditions of a tilt wing V/STOL airplane /$fby James L. Williams
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1972.
215   $a1 online resource (24 pages) $cillustrations
225 1 $aNASA/TN ;$vD-7114
300   $a"December 1972."
320   $aIncludes bibliographical references (page 11).
606   $aAerodynamic coefficients$2nasat
606   $aV/STOL aircraft$2nasat
606   $aAirplanes$xPerformance$vStatistics
606   $aStability of airplanes, Longitudinal
606   $aParameter estimation
606   $aMathematical statistics
606   $aAirplanes$xPerformance$2fast
606   $aConvertiplanes$2fast
606   $aMathematical statistics$2fast
606   $aParameter estimation$2fast
606   $aStability of airplanes, Longitudinal$2fast
608   $aStatistics.$2fast
608   $aStatistics.$2lcgft
615  7$aAerodynamic coefficients.
615  7$aV/STOL aircraft.
615  0$aAirplanes$xPerformance
615  0$aStability of airplanes, Longitudinal.
615  0$aParameter estimation.
615  0$aMathematical statistics.
615  7$aAirplanes$xPerformance.
615  7$aConvertiplanes.
615  7$aMathematical statistics.
615  7$aParameter estimation.
615  7$aStability of airplanes, Longitudinal.
700   $aWilliams$b James L$c(Of Langley Research Center),$08470
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bABC
801  1$bABC
801  2$bOCL
801  2$bAD#
801  2$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bCOP
801  2$bGPO
906   $aBOOK
912   $a9910716530403321
996   $aExtraction of longitudinal aerodynamic coefficients from forward-flight conditions of a tilt wing V$93514308
997   $aUNINA