arXiv (All)
open access
Leading-edge energy transfer governs flutter onset of a pitching finite wing in low-Reynolds number flows
Flutter onset is determined by the sign of the aerodynamic work on the structure, but cycle-integrated work does not reveal where this energy transfer originates. We perform direct numerical simulations of incompressible flow over an aspect-ratio-two NACA 0015 wing pitching at $Re=1000$ and use lobe
Conceptio Open Archive
Analyze & explore related research in Conceptio
Connect this record directly into your research workflow or AI agent. Explore citations across open repositories, query full text, and export structured proof bundles.
This document is indexed with metadata only: full text is not available in the archive for this record. Open the official source ↗
Related documents
- A structure-preserving staggered semi-implicit four-split finite volume scheme for continuum mechanics on unstructured meshes#1061840
- A Numerical Study of Entropy Generation on an Oldroyd-B Nanofluid flow Past a Riga Plate#932688
- Not a Creature Was Stirring#54832
- Scaling Law for Couette-Poiseuille Type Turbulent Flow and Study on 1/2 Power Law and Core Regions#22493
- Water exit dynamics of jumping archer fish: Integrating two-phase flow large-eddy simulation with experimental measurements#630679
Record · ID 1186716
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Bring this data into your agent: Connect via MCP or API · 20 free credits to start · no card required
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive