FAST SOLUTION OF TURBULENT SEPARATION BY STRAWN’S METHOD

FAST SOLUTION OF TURBULENT SEPARATION BY STRAWN’S METHOD

A quasi-simultaneous viscous/inviscid interaction model and a new integral method are tested in connection with the prediction 2D incompressible turbulent separated boundary layer flows. The results are compared with experiments and other predictions. (AIAA)

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Nanjing University of Aeronautics and Astronautics, Transactions (1005-1120) Transactions (1005-1120), 1994-05, Vol.11 (1), p.110-113
1. Verfasser: Yin, Junfei
Format: Artikel
Sprache:eng
Schlagworte:
aerodynamics
boundary
computational
diffuse
flow
interaction
layer
mode
now
separation
trubulent
two-dimensional
viscous/inviscid
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:A quasi-simultaneous viscous/inviscid interaction model and a new integral method are tested in connection with the prediction 2D incompressible turbulent separated boundary layer flows. The results are compared with experiments and other predictions. (AIAA)
ISSN:1005-1120