PHASE RESONANCE METHOD FOR LINEARIZED IDENTIFICATION OF NONLINEAR MECHANICAL STRUCTURES

von Tang, M.
Veröffentlicht in International Forum on Aeroelasticity and Structural Dynamics (19. : 2022 : Madrid) 19th International Forum on Aeroelasticity and Structural Dynamics (IFASD 2022) ; Volume 3 of 4 (2023)

TAXI VIBRATION TESTING: A NEW AND TIME EFFICIENT PROCEDURE FOR THE IDENTIFICATION OF MODAL PARAMETERS ON AIRCRATTS

von Soal, K.
Veröffentlicht in IFASD (18. : 2019 : Savannah, Ga.) International Forum on Aeroelasticity and Structural Dynamics (IFASD 2019) ; Volume 1 of 3 (2020)

ONLINE MONITORING OF FLUTTER STABILITY DURING WIND TUNNEL TESTING OF AN ELASTIC WING WITH PYLON AND ENGINE NACELLE WITHIN THE HMAE1 PROJECT

von Boswald, M.
Veröffentlicht in IFASD (18. : 2019 : Savannah, Ga.) International Forum on Aeroelasticity and Structural Dynamics (IFASD 2019) ; Volume 2 of 3 (2020)

SEMI-AUTONOMOUS ANALYSIS OF LARGE AIRCRAFT GROUND VIBRATION TESTS

von Volkmar, R.
Veröffentlicht in International Forum on Aeroelasticity and Structural Dynamics (19. : 2022 : Madrid) 19th International Forum on Aeroelasticity and Structural Dynamics (IFASD 2022) ; Volume 1 of 4 (2023)

EMBEDDED FLIGHT VIBRATION TESTING SYSTEMFOR ONLINE FLUTTER MONITORING OF UAVS

von Soal, K.
Veröffentlicht in International Forum on Aeroelasticity and Structural Dynamics (19. : 2022 : Madrid) 19th International Forum on Aeroelasticity and Structural Dynamics (IFASD 2022) ; Volume 2 of 4 (2023)

DESIGN AND WIND TUNNEL TEST OF AN ACTIVELY CONTROLLED FLEXIBLE WING

von Kruger, W. R.
Veröffentlicht in IFASD (18. : 2019 : Savannah, Ga.) International Forum on Aeroelasticity and Structural Dynamics (IFASD 2019) ; Volume 2 of 3 (2020)