Dynamic Response of Typical Section Using Variable-Fidelity Fluid Dynamics and Gust-Modeling Approaches—With Correction Methods

Author:

Berci M.1,Mascetti S.2,Incognito A.2,Gaskell P. H.3,Toropov V. V.4

Affiliation:

1. Univ. of Leeds, Leeds LS2 9JT, U.K. (corresponding author).

2. XC Engineering, Cantu’ 22063, Italy.

3. Professor, Univ. of Durham, Durham DH1 3LE, U.K.; formerly, Univ. of Leeds, Leeds LS2 9JT, U.K.

4. Professor, Queen Mary Univ. of London, London E1 4NS, U.K.; formerly, Univ. of Leeds, Leeds LS2 9JT, U.K.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference53 articles.

1. Interpolation Method for Adapting Reduced-Order Models and Application to Aeroelasticity

2. Ansari S. A. (2004). “A nonlinear unsteady aerodynamic model for insect-like flapping wings in the hover with micro air vehicle applications.” Ph.D. thesis Cranfield Univ. U.K.

3. Multifidelity metamodel building as a route to aeroelastic optimization of flexible wings

4. Rotary Wing Structural Dynamics and Aeroelasticity, Second Edition

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