LEADER 01992oam  2200589   450 
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005 20201117104310.0
035   $a(CKB)5470000002507402
035   $a(OCoLC)760986374
035   $a(EXLCZ)995470000002507402
100   $a20111114j196810    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of shape changes on the aerodynamic characteristics of a twisted and cambered arrow wing at Mach number 2.03 /$fby Emma Jean Landrum and Barrett L. Shrout
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dOctober 1968.
215   $a1 online resource (20 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-4796
300   $a"October 1968."
320   $aIncludes bibliographical references (page 7).
606   $aAerodynamics, Supersonic
606   $aCamber (Aerofoils)
606   $aMach number
606   $aReynolds number
606   $aAerodynamics, Supersonic$2fast
606   $aCamber (Aerofoils)$2fast
606   $aMach number$2fast
606   $aReynolds number$2fast
615  0$aAerodynamics, Supersonic.
615  0$aCamber (Aerofoils)
615  0$aMach number.
615  0$aReynolds number.
615  7$aAerodynamics, Supersonic.
615  7$aCamber (Aerofoils)
615  7$aMach number.
615  7$aReynolds number.
700   $aLandrum$b Emma Jean$01404184
702   $aShrout$b Barrett L.
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$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910715060103321
996   $aEffect of shape changes on the aerodynamic characteristics of a twisted and cambered arrow wing at Mach number 2.03$93478353
997   $aUNINA