Work

Slender wings with leading-edge vortex separation - A challenge for panel-methods and Euler-solvers

Year: 1983

Type: conference-paper

Source: AIAA Aerospace Sciences Meeting

DOI: 10.2514/6.1983-562

Authors: S. HITZEL, W. SCHMIDT

Institution: Dornier Flugzeugwerke (Germany)

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W2329488302

FWCI: 1.026

Cites: 7

Cited by: 5

Related to: 10