TY - GEN
T1 - High fidelity trim calculation under consideration of aeroelastic effects of a high aspect ratio swept wing
AU - Hermanutz, Andreas
AU - Hornung, Mirko
N1 - Publisher Copyright:
© 2017 International Forum on Aeroelasticity and Structural Dynamics (IFASD). All Rights Reserved.
PY - 2017
Y1 - 2017
N2 - New structural wing technologies like morphing structures, high aspect ratio wings or passive as well as active load elevation techniques have in common that flexibility is increasing within the next generation of aircraft wings. Therefore, the aeroelastic effects will rise and sophisticated methods are needed to develop and predict the aircrafts properties, load and overall behavior on a highly accurate level. The presented paper shows the work on virtual aircraft models and the application of high fidelity computational fluid structure interaction methods for the development of structural wing design on a high aspect ratio composite wing transport aircraft demonstrator.
AB - New structural wing technologies like morphing structures, high aspect ratio wings or passive as well as active load elevation techniques have in common that flexibility is increasing within the next generation of aircraft wings. Therefore, the aeroelastic effects will rise and sophisticated methods are needed to develop and predict the aircrafts properties, load and overall behavior on a highly accurate level. The presented paper shows the work on virtual aircraft models and the application of high fidelity computational fluid structure interaction methods for the development of structural wing design on a high aspect ratio composite wing transport aircraft demonstrator.
KW - Computational Fluid Structure Interaction
KW - High Aspect Ratio Wings
KW - Structural Wing Design
UR - https://www.scopus.com/pages/publications/85048613089
M3 - Conference contribution
AN - SCOPUS:85048613089
T3 - 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017
BT - 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017
PB - International Forum on Aeroelasticity and Structural Dynamics (IFASD)
T2 - 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017
Y2 - 25 June 2017 through 28 June 2017
ER -