Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
Lock, R.C.
and
Williams, B.R.
1987.
Viscous-inviscid interactions in external aerodynamics.
Progress in Aerospace Sciences,
Vol. 24,
Issue. 2,
p.
51.
ALEMDAROGLU, N.
and
NAKAYAMA, A.
1988.
Measurements of highly asymmetric trailing-edge flow.
Williams, B R
1991.
Viscous-inviscid interaction schemes for external aerodynamics.
Sadhana,
Vol. 16,
Issue. 2,
p.
101.
Yin, Jun-Fei
and
Yu, Shao-Zhi
1993.
Investigation of turbulent separation-reattachement flow in a curved-wall diffuser.
International Journal of Heat and Fluid Flow,
Vol. 14,
Issue. 2,
p.
129.
Wolkov, A. V.
and
Lyapunov, S. V.
1994.
Numerical prediction of transonic viscous separated flow past an airfoil.
Theoretical and Computational Fluid Dynamics,
Vol. 6,
Issue. 1,
p.
49.
Jun-Fei, Y.
and
Shao-Zhi, Y.
1994.
Application of LDV to Investigation of Turbulent Scparation-Reattachment Flow in a Curved-Wall Diffuser.
International Journal of Turbo and Jet Engines,
Vol. 11,
Issue. 1,
Chung, Sang-Tae
Choi, Hyoung Gwon
and
Yoo, Jung Yul
1998.
An analysis of turbulent flow around a NACA4412 airfoil by using a segregated finite element method.
KSME International Journal,
Vol. 12,
Issue. 6,
p.
1194.
Jansen, Kenneth E.
1999.
A stabilized finite element method for computing turbulence.
Computer Methods in Applied Mechanics and Engineering,
Vol. 174,
Issue. 3-4,
p.
299.
Voke, Peter R
and
Yang, Zhiyin
1999.
Industrial and Environmental Applications of Direct and Large-Eddy Simulation.
Vol. 529,
Issue. ,
p.
46.
Yang, Zhiyin
and
Voke, Peter R.
2000.
Large-eddy simulation of separated leading-edge flow in general co-ordinates.
International Journal for Numerical Methods in Engineering,
Vol. 49,
Issue. 5,
p.
681.
Schmidt, Stefan
Franke, Martin
and
Thiele, Frank
2001.
Assessment of SGS models in LES applied to a NACA 4412 airfoil.
Schmidt, S.
and
Thiele, F.
2002.
Advances in LES of Complex Flows.
Vol. 65,
Issue. ,
p.
255.
Maciel, Yvan
Rossignol, Karl-Stéphane
and
Lemay, Jean
2005.
A Study of a Separated Turbulent Boundary Layer in Stalled-Airfoil-Type Flow Conditions.
Maciel, Yvan
Rossignol, Karl-Stéphane
and
Lemay, Jean
2006.
A study of a turbulent boundary layer in stalled-airfoil-type flow conditions.
Experiments in Fluids,
Vol. 41,
Issue. 4,
p.
573.
Peltonen, Risto
2006.
Viscous-Inviscid Method for Airfoil Analysis and Design for Aviation and Windmills.
Journal of Aircraft,
Vol. 43,
Issue. 4,
p.
1069.
Koenig, Benedikt
Fares, Ehab
Jammalamadaka, Avinash
and
Li, Yanbing
2014.
Investigation of the NACA 4412 Trailing Edge Separation Using a Lattice-Boltzmann Approach.
Hosseini, S.M.
Vinuesa, R.
Schlatter, P.
Hanifi, A.
and
Henningson, D.S.
2016.
Direct numerical simulation of the flow around a wing section at moderate Reynolds number.
International Journal of Heat and Fluid Flow,
Vol. 61,
Issue. ,
p.
117.
Knopp, Tobias A.
2016.
A new wall-law for adverse pressure gradient flows and modification of k-omega type RANS turbulence models.
Vinuesa, Ricardo
Hosseini, Seyed M.
Hanifi, Ardeshir
Henningson, Dan S.
and
Schlatter, Philipp
2017.
Pressure-Gradient Turbulent Boundary Layers Developing Around a Wing Section.
Flow, Turbulence and Combustion,
Vol. 99,
Issue. 3-4,
p.
613.
Veldman, Arthur E. P.
2017.
Entrainment and boundary-layer separation: a modeling history.
Journal of Engineering Mathematics,
Vol. 107,
Issue. 1,
p.
5.