000021367 001__ 21367
000021367 005__ 20170522124351.0
000021367 04107 $$aeng
000021367 046__ $$k2017-05-15
000021367 100__ $$aMališ, M.
000021367 24500 $$aSIMULATION OF PILOT LOAD DURING EMERGENCY LANDING CONDITIONS

000021367 24630 $$n23.$$pEngineering Mechanics 2017
000021367 260__ $$bBrno University of Technology, Institute of Solid Mechanics, Mechatronics and Biomechanics, Brno
000021367 506__ $$arestricted
000021367 520__ $$2eng$$aModels of dummy embedded in numerical commercial software packages are calibrated using Anthropometric Testing Dummies (ATD). The dummies vary according to the loading character different for aeronautic or automotive industries. The aim of the article is to find a solution of analysis of loads in lumbar column, based on aeronautical regulation requirements using available dummies in commercial software systems MSC.Nastran and MSC.Dytran. Simulation results were compared with experimental test data obtained from dynamic sled test with implemented ATD.

000021367 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000021367 653__ $$aAircraft passive safety, Finite element method, Dummy, Dynamic test.

000021367 7112_ $$aEngineering Mechanics 2017$$cSvratka, CZ$$d2017-05-15 / 2017-05-18$$gEM2017
000021367 720__ $$aMališ, M.$$iŠplíchal, J.
000021367 8560_ $$ffischerc@itam.cas.cz
000021367 8564_ $$s969773$$uhttps://invenio.itam.cas.cz/record/21367/files/0610.pdf$$yOriginal version of the author's contribution in proceedings, page 610, section DYN.
000021367 962__ $$r21225
000021367 980__ $$aPAPER