Reynolds-number effects in flow around more-or-less bluff bodies

By G. Schewe. 2001

218 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Environmental Engineering

View Paper: https://www.semanticscholar.org/paper/dd8748146be106036d8f2ee6ff1769dc2ad842d4

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Ronald D. Joslin
2. S. Collis
3. Avi Seifert
4. V. Theofilis

In Computational Mechanics

1. Ronald D. Joslin
2. S. Collis
3. Avi Seifert
4. V. Theofilis
5. J. Robinet
6. Peter J. Schmid

In Environmental Engineering

1. Ronald D. Joslin
2. S. Collis
3. Avi Seifert
4. V. Theofilis

Citations in the corpus

• Experimental Study of Shock Oscillation over a Transonic Supercritical Profile (2009, unknown): “D fl ow organizationseemstobetriggeredbythelaminar/turbulenttransition andtodependonitslocationontheairfoil[19],anditcharacterizes anintermediatestatebetweenattached fl ow ( Re (cid:6) 0 : 8 (cid:4) 10 6 , maximum lift) and fully detached fl ow ( Re (cid:6) 7 : 4 (cid:4) 10 6 , lower lift).”
• Issues in active flow control: theory, control, simulation, and experiment (2004, result): “Such structures have also been observed by Schewe [58,59] on his generic airfoil experiment, with periodicity lengths similar to that found on circular cylinders at comparable conditions, as shown in Fig.”
• Advances in global linear instability analysis of nonparallel and three-dimensional flows (2003, background): “Upper: asymmetric cellular structures in transitional flow over an aerofoil [180].”