On the dynamic fluid–structure stability response of an innovative airplane configuration-Reference-Cited by-同舟云学术

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On the dynamic fluid–structure stability response of an innovative airplane configuration

Published:2021-08 Issue: Volume:105 Page:103347
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Bombardieri R.^ORCID,Cavallaro R.,Castellanos R.^ORCID,Auricchio F.

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference63 articles.

1. PARSIFAL project: a breakthrough innovation in air transport;Abu Salem;Aerotec. Missili Spaz.,2018

2. A doublet lattice method for calculating lift distributions on oscillating surfaces in subsonic flows;Albano;AIAA J.,1969

3. Development of a Framework for Unified Flight-Dynamic and Aeroelastic Analysis;Auricchio,2017

4. Unified aeroelastic and flight dynamic formulation via rational function approximations;Baldelli;J. Aircr.,2006

5. Unified longitudinal flight-dynamic and aeroelastic analysis of a prandtlplane configuration;Bombardieri,2017

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1. Nonlinear flutter response and reliability of supersonic smart hybrid nanocomposite rupture trapezoidal plates subjected to yawed flow using DQHFEM;Aerospace Science and Technology;2024-02

2. Sensitivity and uncertainty analysis of the nonlinear flight dynamics system of the flexible body;Aerospace Science and Technology;2023-08

3. Engine Placement Effects on the Flutter of a Medium-Range Box-Wing Aircraft;Journal of Aerospace Engineering;2023-07

4. Unconventional aircraft for civil aviation: A review of concepts and design methodologies;Progress in Aerospace Sciences;2022-05

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