To determine allowable tolerances between successive suction panels at hybrid laminar wings with suction surfaces, direct numerical simulations of Tollmien–Schlichting waves over different steps are carried out for realistic suction rates on a wind tunnel configuration. Simulations at given suction panel positions over forward and backward facing steps are carried out by the use of a high-order method for the direct simulation of Tollmien–Schlichting wave growth. Comparisons between high-fidelity direct numerical simulations and quick linear stability calculations have shown capabilities and limits of the well-validated linear stability theory design approach.
Direct numerical simulation of TS-waves over suction panel steps from manufacturing tolerances
CEAS Aeronaut J
CEAS Aeronautical Journal ; 12 , 2 ; 261-271
2021-04-01
11 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Emerald Group Publishing | 1939
|Influence of manufacturing tolerances
Online Contents | 1994
|Direct Numerical Simulation of Turbulent Transport with Uniform Wall Injection and Suction
Online Contents | 1995
|