ADJOINT-BASED MESH ADAPTATION FOR DIRECT FLUTTER PREDICTION
Kevin G. Wang, Philip S. Beran, Shunxiang Cao
DOI Number: N/A
Conference number: IFASD-2017-212
MULTIDISCIPLINARY DESIGN OPTIMIZATION OF WING STRUCTURE FOR STRUT-BRACED WING AIRCRAFT CONSIDERING AEROELASTICITY
Wang Zexi, Wan Zhiqiang, Yang Chao, Zhu Siyan
DOI Number: N/A
Conference number: IFASD-2017-210
AN INTEGRATED OPTIMIZATION AND SURROGATE ANALYSIS OF LARGE AIRCRAFT IN CONCEPTUAL DESIGN
Xiaozhe Wang, Zhiqiang Wan, Chao Yang
DOI Number: N/A
Conference number: IFASD-2017-209
COMPARISON OF AERODYNAMIC MODELS FOR 1-COSINE GUST LOADS PREDICTION
Christopher Wales, R. G. Cook, D. P. Jones, A. L. Gaitonde
DOI Number: N/A
Conference number: IFASD-2017-208
THE AEROELASTIC BEHAVIOUR OF A FORWARD-SWEPT WING CONFIGURATION WITH FOCUS ON ENGINE GYROSCOPICS AND T-TAIL FLUTTER
Stefan Waitz
DOI Number: N/A
Conference number: IFASD-2017-207
DYNAMIC MANEUVER LOADS CALCULATION FOR A SAILPLANE AND COMPARISON WITH FLIGHT TEST
Arne Voß, Gabriel Pinho Chiozzotto, Per Ohme
DOI Number: N/A
Conference number: IFASD-2017-206
EFFICIENT AND ACCURATE AEROELASTIC ANALYSES BASED ON SMALL-DISTURBANCE CFD IN EARLY AIRCRAFT DEVELOPMENT
Cyrille Vidy, Lukas Katzenmeier, Maximilian Winter, Christian Breitsamter
DOI Number: N/A
Conference number: IFASD-2017-205
FREEPLAY-INDUCED LIMIT CYCLE OSCILLATION MITIGATION USING LINEAR AND NONLINEAR TUNED VIBRATION ABSORBERS
E. Verstraelen, G. Kerschen, G. Dimitriadis
DOI Number: N/A
Conference number: IFASD-2017-204
AN OPTIMIZED DOUBLET-LATTICE METHOD CORRECTION APPROACH FOR A LARGE CIVIL AIRCRAFT
C. Valente, C. Wales, D. Jones, A. Gaitonde, J. E. Cooper, Y. Lemmens
DOI Number: N/A
Conference number: IFASD-2017-200
DESIGN OF AN INNOVATIVE WING TIP DEVICE
F. Toffol, F. Fonte, S. Ricci
DOI Number: N/A
Conference number: IFASD-2017-198