The method of Lees-Reeves-Klineberg has been successful for rapidly predicting a large class of interacting laminar flows. Hunter and Reeves extended the laminar work and presented a method for calculating the two-dimensional flow separation and reattachment of a turbulent boundary layer caused by a compression corner. In this work, a further extension is made to supersonic turbulent flows over adiabatic two-dimensional compression corners where the turning angle is such that the flow remains attached. The importance of the problem coupled with the success of the moment for similar flows strongly suggests its development for applications where rapid calculations are essential. (Kursetz)
Correlation technique for predicting attached turbulent boundary - layer/flap interaction pressures
Korrelationsmethode zur Vorbestimmung der Wechselwirkungsdruecke von Begleitturbulenz-Grenzschichten an Klappen
AIAA Journal ; 18 , 1 ; 9-10
1980
2 Seiten, 3 Bilder, 6 Quellen
Article (Journal)
English