LEADER 01795nam  2200493I  450 
001 9910707343903321
005 20160721125257.0
035   $a(CKB)5470000002464080
035   $a(OCoLC)953832995
035   $a(EXLCZ)995470000002464080
100   $a20160721j201604    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCompressive testing of stitched frame and stringer alternate configurations /$fFrank A. Leone, Jr., Dawn C. Jegley
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dApril 2016.
215   $a1 online resource (iv, 27 pages)$ccolor illustrations
225 1 $aNASA/TM ;$v2016-218974
300   $aTitle from title screen (viewed July 21, 2016).
300   $a"April 2016."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 26-27).
606   $aBody-wing configurations$2nasat
606   $aComposite structures$2nasat
606   $aFuselages$2nasat
606   $aStringers$2nasat
606   $aTransport aircraft$2nasat
615  7$aBody-wing configurations.
615  7$aComposite structures.
615  7$aFuselages.
615  7$aStringers.
615  7$aTransport aircraft.
700   $aLeone$b Frank A.$01399025
702   $aJegley$b Dawn C.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707343903321
996   $aCompressive testing of stitched frame and stringer alternate configurations$93493999
997   $aUNINA