A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures

Vanzulli, Mauricio C.; Pérez Zerpa, Jorge M.

doi:10.1016/j.heliyon.2023.e19990

Heliyon

2023

DOI: 10.1016/j.heliyon.2023.e19990

|View full text |Cite

A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures

Mauricio C. Vanzulli,

Jorge M. Pérez Zerpa

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

Supporting

Mentioning

Contrasting

Year Published

2024

2025

Publication Types

Select...

Article3

Relationship

Self Cite0

Independent3

Authors

Journals

Cited by 3 publications

References 43 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

Simulating flow-induced reconfiguration by coupling corotational plate finite elements with a simplified pressure drag

Lamoureux,

Ramananarivo,

Melancon

et al. 2025

Extreme Mechanics Letters

View full text Add to dashboard Cite

Simulating flow-induced reconfiguration by coupling corotational plate finite elements with a simplified pressure drag

Lamoureux,

Ramananarivo,

Melancon

et al. 2025

Extreme Mechanics Letters

View full text Add to dashboard Cite

Modeling vortex-induced vibrations of branched structures by coupling a 3D-corotational frame finite element formulation with wake-oscillators

Villié,

Vanzulli,

Zerpa

et al. 2024

Journal of Fluids and Structures

View full text Add to dashboard Cite

Effects of Propeller Distribution on the Aeroelastic Characteristics of Large-Deformation Wings

Wu,

Zhou,

Wang

2024

Aerospace

View full text Add to dashboard Cite

Considering the large-deformation and multi-propeller characteristics of very flexible aircraft, propeller effects are introduced and accessed in the wing static and dynamic aeroelastic analysis and different propeller distributions are utilized to obtain more aeroelastic benefits. The propeller–wing aeroelastic interactions are innovatively modeled in the paper. For propeller–wing aerodynamic interaction, propeller-induced velocities are considered and added in the nonplanar steady and unsteady vortex lattice methods. For propeller–wing structural interaction, the conversion of loads and displacements between attached propellers and the large-deformation wing is derived. Static aeroelastic cases indicate that thrust can reduce structural deformation and slipstream can cause considerable lift increment. Dynamic cases indicate that thrust can reduce the wing’s maximum response to gust and bring an improvement of 9.4% in the wing’s critical velocity, while slipstream can reduce the gust response amplitude. In addition, using smaller and more propellers is recommended instead of an individual larger propeller. Decreasing and increasing propeller speeds toward the wingtip is more beneficial for cruise status and gust alleviation, respectively.

show abstract

scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.

Contact Info

customersupport@researchsolutions.com

10624 S. Eastern Ave., Ste. A-614

Henderson, NV 89052, USA

This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.

Blog Terms and Conditions API Terms Privacy Policy Contact Cookie Preferences Do Not Sell or Share My Personal Information

Made with 💙 for researchers

Part of the Research Solutions Family.

A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures

Cited by 3 publications

References 43 publications

Simulating flow-induced reconfiguration by coupling corotational plate finite elements with a simplified pressure drag

Simulating flow-induced reconfiguration by coupling corotational plate finite elements with a simplified pressure drag

Modeling vortex-induced vibrations of branched structures by coupling a 3D-corotational frame finite element formulation with wake-oscillators

Effects of Propeller Distribution on the Aeroelastic Characteristics of Large-Deformation Wings

Contact Info

Product

Resources

About