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100   $a20130912j199909    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air /$fWilliam I. Scallion
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dSeptember 1999.
215   $a1 online resource (54 pages) $cillustrations
225 1 $aNASA TM- ;$v1999-209357
300   $a"September 1999."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 9).
606   $aControllability$2nasat
606   $aEffectiveness$2nasat
606   $aLifting bodies$2nasat
606   $aScale models$2nasat
606   $aWind tunnel tests$2nasat
606   $aElevons$2nasat
615  7$aControllability.
615  7$aEffectiveness.
615  7$aLifting bodies.
615  7$aScale models.
615  7$aWind tunnel tests.
615  7$aElevons.
700   $aScallion$b William I.$01395362
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910706169003321
996   $aAerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air$93453744
997   $aUNINA