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    Correction to: Aircraft noise generation and assessment

    Bertsch, L. / Snellen, M. / Enghardt, L. et al. | Online Contents | 2019
    The original version of below mentioned articles was unfortunately published with the special issue titleAircraft noise generation and ...

    Bilevel Optimization Strategy for Aircraft Wing Design Using Parallel Computing

    Elham, Ali / Tooren, Michel J.L. van / Sobieszczanski-Sobieski, Jaroslaw | Tema Archive | 2014
    A new bilevel optimization strategy for wing design is developed, in which the optimizations of the wing-planform and wing-airfoil shapes ...

    Scalable parallel approach for high-fidelity steady-state aeroelastic analysis and adjoint derivative computations

    Kenway, Gaetan K. / Kennedy, Graeme J. / Martins, Joaquim R.R.A. | Tema Archive | 2014
    parallel scalability of the methods is demonstrated for a full aircraft configuration using an Euler computational fluid dynamics model with more ...

    Weight Indexing for Wing-Shape Multi-Objective Optimization

    Elham, Ali / Tooren, Michel J.L. van | Tema Archive | 2014
    maximum takeoff weight and the aircraft direct operating cost are used as the design figures of merit to identify the best wings among the wings ...

    Flutter failure risk assessment for damage-tolerant composite aircraft structures

    Styuart, Andrey V. / Livne, Eli / Demasi, Luciano et al. | Tema Archive | 2011
    A method for quantifying the reliability and damage tolerance of aircraft composite structures due to flutter in the presence of multiple ...

    Modeling and simulation of nonlinear dynamics of flapping wing micro air vehicles

    Orlowski, Christopher T. / Girard, Anouck R. | Tema Archive | 2011
    The derivation of the nonlinear dynamics of flapping wing micro air vehicles is presented. Simulation results investigate differences in ...

    Analysis of conformable pressure vessels: introducing the multibubble

    Geuskens, F.J.J.M.M. / Bergsma, O.K. / Koussios, S. et al. | Tema Archive | 2011
    This paper outlines the structural analysis of an articulated pressurizable structure termed the multibubble. The multibubble is a ...

    Comparison of surrogate models in a multidisciplinary optimization framework for wing design

    Paiva, Ricardo M. / Carvalho, Andre R.D. / Crawford, Curran et al. | Tema Archive | 2010
    response surfaces, Kriging, and artificial neural networks. The results obtained from the solution of four different case studies based on aircraft ...

    Harmonic-balance-based code-coupling algorithm for aeroelastic systems subjected to forced excitation

    Blanc, F. / Roux, F.X. / Jouhaud, J.C. | Tema Archive | 2010
    an aircraft wing is taken into account in the computation of unsteady aerodynamic forces caused by an oscillating aileron. ...

    Surrogate modeling for uncertainty assessment with application to aviation environmental system models

    Allaire, D. / Willcox, K. | Tema Archive | 2010
    surrogate predictions. The approach is developed for a general class of models and is demonstrated on an aircraft emissions prediction model that is ...

    High-lift airfoil separation with dielectric barrier discharge plasma actuation

    Little, Jesse / Samimy, Mo | Tema Archive | 2010
    The efficacy of a single dielectric barrier discharge plasma actuator for controlling turbulent boundary-layer separation from the ...

    Topological optimization of compliant adaptive wing structure

    Santer, M. / Pellegrino, S. | Tema Archive | 2009
    Load-path-based topology optimization is used to synthesize a compliant adaptive aircraft wing leading edge, which deforms in a prescribed ...

    Active aeroelastic control over a multisurface wing: modeling and wind-tunnel testing

    Gaspari, A. de / Ricci, S. / Riccobene, L. et al. | Tema Archive | 2009
    a roll maneuver enhancement control system, now under development, so to be able to optimize the aircraft roll performances in terms of both ...

    Design and modeling of selective reinforcements for integral aircraft structures

    Boscolo, Marco / Allegri, Giuliano / Zhang, Xiang | Tema Archive | 2008
    A numerical simulation is presented in this paper on the performance of crack retarders bonded to integral metallic structures. The work is ...

    Optimization of aircraft wings for gust loads: interval analysis-based approach

    Rao, S.S. / Majumder, Luna | Tema Archive | 2008
    An interval-based approach is presented for the optimization of aircraft structures under dynamic loads. As a specific application, the ...

    Efficient Parallel Algorithm for multiconstrained of wing body configurations

    Peigin, S. / Epstein, B. | Tema Archive | 2008
    Three-Dimensional Wings Driven by Navier-Stokes Computations', AIAA Journal, Vol. 43, No. 9, 2005, pp.1946-1957.]. In industry, the success of ...

    Efficient approach for multipoint aerodynamic wing design of business jet aircraft

    Epstein, Boris / Peigin, Sergey | Tema Archive | 2007
    design of three-dimensional isolated wings. In the framework of the method, the total drag of an optimized aircraft configuration is minimized at ...

    Low-frequency acoustic shielding by the silent aircraft airframe

    Agarwal, Anurag / Dowling, Ann P. | Tema Archive | 2007
    The 'Silent Aircraft Initiative' is a project funded by the Cambridge-MIT Institute (CMI). Its aim is to discover ways of reducing aircraft ...

    Measurement and prediction of noise propagation from a high-power jet aircraft

    Gee, Kent L. / Sparrow, Victor W. / James, Michael M. et al. | Tema Archive | 2007
    the deployment of next-generation fighter aircraft. An amplitude-dependent wave speed, neglected as part of linear acoustics assumptions ...

    Aerodynamic optimization of a morphing airfoil using energy as an objective

    Namgoong, Howoong / Crossley, William A. / Lyrintzis, Anastasios S. | Tema Archive | 2007
    Recent advances in materials science and actuation technologies have raised interest in morphing aircraft that can significantly change ...