UFR 2-11 Test Case

From KBwiki
Jump to navigation Jump to search

High Reynolds Number Flow around Airfoil in Deep Stall

Front Page

Description

Test Case Studies

Evaluation

Best Practice Advice

References

Flows Around Bodies

Underlying Flow Regime 2-11

Test Case Study

Brief Description of the Test Case

The following presents a precise description of the primary test case, the NACA0021 airfoil at 60° angle of attack.


A visual impression of the geometry and flow has been shown in Figure 1. The experiments were carried out in the wind tunnel of Monash University (see Figure 2). The width of the experimental section is 7.2 airfoil chord lengths, c, and its height is 16c.


UFR2-11 figure2a.jpg|UFR2-11 figure2b.gif
Figure 2: NACA0021 airfoil in wind tunnel (left) and a plan view of wind tunnel (right) []

Test Case Experiments

CFD Methods




Contributed by: Charles Mockett; Misha Strelets — CFD Software GmbH and Technische Universitaet Berlin; New Technologies and Services LLC (NTS) and Saint-Petersburg State University

Front Page

Description

Test Case Studies

Evaluation

Best Practice Advice

References


© copyright ERCOFTAC 2024