arXiv (OAI Expanded)
open access
An analysis of aerodynamic properties of delta wings
We consider a sharp-edge delta wing of small aspect ratio $A>0$, which is an example of a 3D airfoil whose aerodynamic properties cannot be modeled using the potential lift}only. An important role is played by a pair of attached vortices, which generate the vortex lift. We review in detail the leadi
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
- Aerodynamic derivatives for a delta wing oscillating in elastic modes#491522
- On the laminar boundary layer separation from the leading edge of a thin aerofoil#491572
- Holonomy Separation and Anyonic Hair in AdS$_3$#1077490
- Dirichlet–Voronoi domain and injectivity radius of flag manifolds — equivariant cell structure on O(3)∕O(1)3#337662
- Ghost polygons, Poisson bracket and convexity#677308
Record · ID 1109986
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