LEADER 01586oam  2200445   450 
001 9910716529303321
005 20210701112138.0
035   $a(CKB)5470000002522865
035   $a(OCoLC)890693636
035   $a(EXLCZ)995470000002522865
100   $a20140916j197212    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNumerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation /$fby Russell B. Sorrells and David S. Miller
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1972.
215   $a1 online resource (47 pages) $cillustrations
225 1 $aNASA/TN ;$vD-7097
300   $a"December 1972."
320   $aIncludes bibliographical references (page 21).
606   $aAerodynamics$2nasat
606   $aCamber$2nasat
606   $aWings$2nasat
615  7$aAerodynamics.
615  7$aCamber.
615  7$aWings.
700   $aSorrells$b Russell B.$01414584
702   $aMiller$b David S$c(Of Langley Research Center),
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716529303321
996   $aNumerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation$93514307
997   $aUNINA