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100   $a20111114j198012    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLeading-edge deflection optimization for a highly swept arrow-wing configuration /$fPaul L. Coe, Jr., Jarrett K. Huffman, and James W. Fenbert
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dDecember 1980.
215   $a1 online resource (56 pages) $cillustrations
225 1 $aNASA technical paper ;$v1777
300   $aTitle from title screen (viewed on Aug. 25, 2016).
300   $a"December 1980."
300   $a"Performing Organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 55-56).
606   $aAerodynamics$2fast
606   $aAirplanes$xWings, Swept-back$2fast
606   $aLeading edges (Aerodynamics)$2fast
615  7$aAerodynamics.
615  7$aAirplanes$xWings, Swept-back.
615  7$aLeading edges (Aerodynamics)
700   $aCoe$b Paul L.$01401937
702   $aHuffman$b Jarrett K.
702   $aFenbert$b James W.
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910707439703321
996   $aLeading-edge deflection optimization for a highly swept arrow-wing configuration$93471390
997   $aUNINA