TY - GEN
T1 - Preliminary validation of a coupled model of nonlinear aeroelasticity and flight dynamics for HALE aircraft
AU - Zhang, Jian
AU - Xiang, Jinwu
PY - 2010
Y1 - 2010
N2 - A coupled model of aeroelasticity and flight dynamics for high-altitude, long-endurance (HALE) aircraft is under development based on the geometrically exact, fully intrinsic beam theory, ONERA aerodynamic stall model, and six degrees of freedom model of rigid body motion. The correlation among the present model, MSC/Nastran, UM/NAST, and NATASHA was studied, including the cases of static equilibrium and forced vibration of a split beam system and trim of a Flying-Wing aircraft. The preliminary validation indicates that the present model is effective in modeling a split beam system and the trim of HALE aircraft.
AB - A coupled model of aeroelasticity and flight dynamics for high-altitude, long-endurance (HALE) aircraft is under development based on the geometrically exact, fully intrinsic beam theory, ONERA aerodynamic stall model, and six degrees of freedom model of rigid body motion. The correlation among the present model, MSC/Nastran, UM/NAST, and NATASHA was studied, including the cases of static equilibrium and forced vibration of a split beam system and trim of a Flying-Wing aircraft. The preliminary validation indicates that the present model is effective in modeling a split beam system and the trim of HALE aircraft.
UR - https://www.scopus.com/pages/publications/79952180929
U2 - 10.1109/ISSCAA.2010.5633261
DO - 10.1109/ISSCAA.2010.5633261
M3 - 会议稿件
AN - SCOPUS:79952180929
SN - 9781424460441
T3 - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
SP - 1411
EP - 1416
BT - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
T2 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010
Y2 - 8 June 2010 through 10 June 2010
ER -