LEADER 01898oam  2200565   450 
001 9910705768203321
005 20170619084440.0
035   $a(CKB)5470000002452723
035   $a(OCoLC)846145815
035   $a(EXLCZ)995470000002452723
100   $a20130602j199712    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAnalysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft /$fVladislav Klein [and three others]
210   $aHampton, Virginia $cNational Aeronautics and Space Administration, Langley Research Center$dDecember 1997
215   $a1 online resource (63 pages) $cillustrations
225 1 $aNASA/TM ;$v97-206276
300   $a"December 1997."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical reference (page 15).
606   $aAerodynamic coefficients$2nasat
606   $aAngle of attack$2nasat
606   $aControl surfaces$2nasat
606   $aF-16 aircraft$2nasat
606   $aFourier series$2nasat
606   $aHarmonic analysis$2nasat
606   $aWind tunnel tests$2nasat
615  7$aAerodynamic coefficients.
615  7$aAngle of attack.
615  7$aControl surfaces.
615  7$aF-16 aircraft.
615  7$aFourier series.
615  7$aHarmonic analysis.
615  7$aWind tunnel tests.
700   $aKlein$b Vladislav$01385898
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910705768203321
996   $aAnalysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft$93448963
997   $aUNINA