Nonlinear Aeroelastic Response of Highly Flexible Flying Wing Due to Different Gust Loads

doi 10.5772/intechopen.75804
Full Text
Abstract

Available in full text

Date
Authors
Publisher

InTech

Related search

Design and Sizing of an Aeroelastic Composite Model for a Flying Wing Configuration With Maneuver, Gust, and Landing Loads

CEAS Aeronautical Journal
TransportationAerospace Engineering
2020English

Nonlinear Aeroelastic Modeling of a Flexible Wing and Comparison With Experiments

English

Aeroelastic Response of a Rigid Wing Supported by Nonlinear Springs

Journal of Aircraft
Aerospace Engineering
1998English

Nonlinear Aeroelastic Analysis of Joined-Wing Aircraft

2003English

Iterative Learning Control of a Nonlinear Aeroelastic System Despite Gust Load

International Journal of Aerospace Engineering
Aerospace Engineering
2015English

Ground Vibration Tests on a Flexible Flying Wing Aircraft - Invited

2016English

Aeroelastic Response Characteristics of a Hovering Rotor Due to Harmonic Blade Pitch Variation.

Journal of the Japan Society for Aeronautical and Space Sciences
1988English

Nonlinear Unsteady Reduced Order Models Based on Computational Fluid Dynamics for Gust Loads Predictions

2018English

X-Hale: A Very Flexible Unmanned Aerial Vehicle for Nonlinear Aeroelastic Tests

AIAA Journal
Aerospace Engineering
2012English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy