01590cam a22004217a 4500001000800000005001700008007001400025008004100039035002300080035001200103037002200115040000900137074001600146086002000162091000800182100002200190245013200212260017500344300000900519490002700528500003400555500005500589533010700644650002800751650003400779650002200813650002500835650002500860650003500885650002000920650002300940650004500963650003201008700002401040710002901064830004101093984003401134414852120080608085204.0he bmb---bbca991103s1999 vau b f000 0 eng d a(OCoLC)ocm42758525 a4148521 a19990036755bNASA a GPO a0830-D (MF)0 aNAS 1.15:209132 amfm1 aJackson, Karen E.10aCrashworthy evaluation of a 1/5-scale model composite fuselage concepth[microform] /cKaren E. Jackson and Edwin L. Fasanella. aHampton, Va. :bNational Aeronautics and Space Administration, Langley Research Center ;a[Springfield, Va. :bNational Technical Information Service, distributor,c1999] a1 v.1 aNASA/TM ;v1999-209132 aShipping list no.: 99-0729-M. aDistributed to depository libraries on microfiche. aMicrofiche.b[Washington, D.C. :cNational Aeronautics and Space Administration,d1999]e1 microfiche. 7aCrashworthiness.2nasat 7aFinite element method.2nasat 7aFuselages.2nasat 7aImpact tests.2nasat 7aScale models.2nasat 7aStructural reliability.2nasat 7aCrashes.2nasat 7aDrop tests.2nasat 7aApplications programs (Computers)2nasat 7aComposite materials.2nasat1 aFasanella, Edwin L.2 aLangley Research Center. 0aNASA technical memorandum ;v209132. aANLcmc SUDOC NAS 1.15:209132