TY - GEN
T1 - Analysis of progressive dynamic damage caused by large hailstone ingestion into modern high bypass turbofan engine
AU - Song, Yangkun
AU - Bayandor, Javid
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2016
Y1 - 2016
N2 - Foreign Object Ingestion is one of the major concerns for the aviation industry. The impact caused by an ingested object can immediately initiate damage within the propulsion system and compromise its functionality. In addition to structural damage, the stability of the engine can also be adversely affected as the compressor is driven to stall due to massive debris ingestion. Among many potential projectiles, hailstone is a candidate that can interact with the engine at any altitude. Ice possesses highly non-linear material properties, with these properties being extremely sensitive to many environmental attributes, including temperature, pressure, and accretion rate. Such complexities make it challenging to numerically predict the ice-structure interaction. In this study, the non-linear behavior of ice was numerically simulated using a finite element framework and compared against physical experiments. The validated methodology was then utilized to investigate, damage initiation, full dynamic response, and failure evolution in a propulsion system subject to ice ingestion.
AB - Foreign Object Ingestion is one of the major concerns for the aviation industry. The impact caused by an ingested object can immediately initiate damage within the propulsion system and compromise its functionality. In addition to structural damage, the stability of the engine can also be adversely affected as the compressor is driven to stall due to massive debris ingestion. Among many potential projectiles, hailstone is a candidate that can interact with the engine at any altitude. Ice possesses highly non-linear material properties, with these properties being extremely sensitive to many environmental attributes, including temperature, pressure, and accretion rate. Such complexities make it challenging to numerically predict the ice-structure interaction. In this study, the non-linear behavior of ice was numerically simulated using a finite element framework and compared against physical experiments. The validated methodology was then utilized to investigate, damage initiation, full dynamic response, and failure evolution in a propulsion system subject to ice ingestion.
UR - https://www.scopus.com/pages/publications/84958582473
M3 - Conference contribution
AN - SCOPUS:84958582473
SN - 9781624103926
T3 - 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
BT - 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2016
Y2 - 4 January 2016 through 8 January 2016
ER -