Publication Date:
2019-07-13
Description:
A gas-act,uated penetration device has been developed for high-energy impact testing of structures. The high-energy impact. t,estiiig is for experimental simulation of uncontained engine failures. The non-linear transient finite element, code LS-DYNA3D has been used in the numerical simula.tions of a titanium rectangular blade with a.n aluminum target, plate. Threshold velocities for different combinations of pitch and yaw angles of the impactor were obtained for the impactor-target, t8est configuration in the numerica.1 simulations. Complet,e penet,ration of the target plate was also simulat,ed numerically. Finally, limited comparison of analytical and experimental results is presented for complete penetration of the target by the impactor.
Keywords:
Aircraft Design, Testing and Performance
Type:
AIAA Paper 99-1385
,
AIAA/ASME/ASCE/AHS/ASC 40th Structures, Structural Dynamics, and Materials Conference; Apr 12, 2004 - Apr 15, 2004; Saint Louis, MO; United States
Format:
application/pdf
