TY - GEN
T1 - Active flow control of complex configurations
AU - Minasyan, Artur
AU - Sidilkover, David
AU - Seifert, Avi
PY - 2014
Y1 - 2014
N2 - A flow analysis and boundary layer control were applied to an inlet shape design that is efficient from the external aerodynamic point of view, but due to its short and high offset suffers from internal flow separations and significant engine face distortions. For simplicity, low Reynolds number and low (practically incompressible) Mach number experiments and simulations were performed on an equivalent 2D geometry. Qualitative agreement was found between experiments and simulations. Preliminary efforts to control this complex flow are presented and tested both by experiments and simulations.
AB - A flow analysis and boundary layer control were applied to an inlet shape design that is efficient from the external aerodynamic point of view, but due to its short and high offset suffers from internal flow separations and significant engine face distortions. For simplicity, low Reynolds number and low (practically incompressible) Mach number experiments and simulations were performed on an equivalent 2D geometry. Qualitative agreement was found between experiments and simulations. Preliminary efforts to control this complex flow are presented and tested both by experiments and simulations.
UR - http://www.scopus.com/inward/record.url?scp=84904889705&partnerID=8YFLogxK
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AN - SCOPUS:84904889705
SN - 9781632662651
T3 - 54th Israel Annual Conference on Aerospace Sciences 2014
SP - 395
EP - 410
BT - 54th Israel Annual Conference on Aerospace Sciences 2014
PB - Technion Israel Institute of Technology
T2 - 54th Israel Annual Conference on Aerospace Sciences, IACAS 2014
Y2 - 19 February 2014 through 20 February 2014
ER -