Flight control design to improve aircraft performance by reducing the flutter and dynamic loads margins
L.Benassi
DOI Number: N/A
Conference number: IFASD-2017-014
Structural design of wing tip part from aeroelasticity consideration
K.Balunov, V.Chedrik, F.Ishmuratov
DOI Number: N/A
Conference number: IFASD-2017-011
Aerodynamic and Structural Design Studies for Fuel Consumption Reduction on Subsonic Aircraft
H.Arizono, D.Kwak, T.Nomura
DOI Number: N/A
Conference number: IFASD-2017-008
Computational Fluid Dynamics Based Aeroelastic System Identification and Flutter Prediction
M.Argaman, D.E.Raveh
DOI Number: N/A
Conference number: IFASD-2017-007
Airbus Defence and Space AWACS PROTOTYPES: AWACS-DOME AEROELASTIC AND DYNAMIC LOADS CHALLENGES
F.Arévalo, M.R.Guitián, P.M.López, J.L.P.Galán, H.Climent
DOI Number: N/A
Conference number: IFASD-2017-006
A method for predicting multivariate random loads and a discrete appoximation of the mutidimensional design load envelope
C.Aquilini, D.Parisse
DOI Number: N/A
Conference Number: IFASD-2017-005
Validation and evaluation of a nonlinear aeroelastic framework using flight test data
F. Afonso, J. Vale, É. Oliveira and F. Lau, F. Moreira, J. Marra, A. Meinicke, M. Pedras, O. Mello, J. Richards, W. Brussow, S. Warwick, A. Suleman
DOI Number: N/A
Conference number: IFASD-2017-004
Experimental and Numerical Simulations of NACA 0018 Airfoil undergoing Stall Flutter with Structural Nonlinearity
A.F. Razaami, M.K.H.M. Zorkipli, N.A.Razak
DOI Number: N/A
Conference number: IFASD-2017-003
Comparison of High-Fidelity Aero-Structure Gradient Computation Techniques. Application on the CRM Wing Design.
T. Achard, C. Blondeau and R. Ohayon
DOI Number: N/A
Conference number: IFASD-2017-002
A Study on the Mechanical Properties and Microwave Absorption Performance of Nickel-coated Basalt Fiber/aluminosilicate Ceramic Composite Applicable to Hypersonic Vehicle
Kwonwoo PARK, Hoyoung SHIN, Dongjun HONG, Hyunseok KO, Jinhwe KWEON, Youngwoo NAM, Byeongsu KWAK
DOI Number: XXX-YYY-ZZZ
Conference number: HiSST-2024-183