TY - GEN
T1 - Multiscale modeling of the radar signature of a composite aircraft
AU - Zhang, Kedi
AU - Jin, Jian Ming
AU - Geubelle, Philippe H.
N1 - Publisher Copyright:
© 2015, American Institute of Aeronautics and Astronautics. All Rights Reserved.
PY - 2015
Y1 - 2015
N2 - A two-step approach consisting of meso- and macro-scale simulations is presented to predict the radar signature of a composite aircraft. At the meso-scale, we develop an efficient method to extract the effective anisotropic surface impedances (ASI), which mimic the electromagnetic properties of composite materials for all incident angles and all polarizations of a radar plane wave at the frequency of interest. The approach is based on an Interface-enriched Generalized Finite Element Method (IGFEM), which uses a virtual model composed of finite elements that do not need to conform with material interfaces, yet provides the same level of accuracy as conforming meshes. At the macro-scale, we employ the extracted ASI to construct a well-conditioned surface integral equation (SIE) to predict the radar signature of the whole aircraft. We implement a parallel Multilevel Fast Multipole Algorithm (MLFMA) to reduce the computational complexity and speed up the process of solving the derived SIE.
AB - A two-step approach consisting of meso- and macro-scale simulations is presented to predict the radar signature of a composite aircraft. At the meso-scale, we develop an efficient method to extract the effective anisotropic surface impedances (ASI), which mimic the electromagnetic properties of composite materials for all incident angles and all polarizations of a radar plane wave at the frequency of interest. The approach is based on an Interface-enriched Generalized Finite Element Method (IGFEM), which uses a virtual model composed of finite elements that do not need to conform with material interfaces, yet provides the same level of accuracy as conforming meshes. At the macro-scale, we employ the extracted ASI to construct a well-conditioned surface integral equation (SIE) to predict the radar signature of the whole aircraft. We implement a parallel Multilevel Fast Multipole Algorithm (MLFMA) to reduce the computational complexity and speed up the process of solving the derived SIE.
UR - http://www.scopus.com/inward/record.url?scp=85086054296&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85086054296&partnerID=8YFLogxK
U2 - 10.2514/6.2015-0703
DO - 10.2514/6.2015-0703
M3 - Conference contribution
AN - SCOPUS:85086054296
T3 - 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
BT - 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015
Y2 - 5 January 2015 through 9 January 2015
ER -