Enlighten Publications
metadata only
Numerical Simulations of a Heavy-lift eVTOL
Simulations of a multi-rotor eVTOL aircraft at high disk-loading condition were undertaken in hovering flight using a viscous vortex particle method combined with a lifting-line blade model. Constant-source panels were used to introduce the influence of the airframe in the solution. Comparisons with
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 New Approach to Comprehensive Rotorcraft Aeromechanics Simulation#283876
- Aeroelastic Simulation of a Hingeless Model Rotor with a Flexible Multibody Model#279838
- ELWIRA: Flying robot platform for control, guidance and mission experiments#291267
- Analysis of the Aeroacoustic Performance of Twin Propellers in Hover by Using the Cira-Cusano Test Rig#1038832
- Simulation of the Free Flying Helicopter by Coupling of a New Comprehensive Aeromechanics Code with an Advanced Flexible Multibody Model#279828
Record · ID 1000545
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