Next: About this document ...
Up: Computational Modeling of the
Previous: Acknowledgment
- 1
-
R.H. Liebeck.
Design of subsonic airfoils for high lift.
Journal of Aircraft, 15(9), 1978.
- 2
-
C.S. Jang, J.C. Ross and R.M. Cummings.
Numerical investigation of an airfoil with a Gurney flap.
Aircraft Design, 1, 1998.
- 3
-
D. Jeffrey and X. Zhang.
Aerodynamics of Gurney flaps on a single-element high-lift wing.
Journal of Aircraft, 37(2), 2000.
- 4
-
J.C. Ross, B.L. Storms and P.G. Carrannanto.
Lift-enhancing tabs on multi-element airfoils.
Journal of Aircraft, 32(3), 1995.
- 5
-
P.G. Carrannanto, B.L. Storms, J.C. Ross and R.M. Cummings.
Navier-Stokes analysis of lift-enhancing tabs on multi-element
airfoils.
Aircraft Design, 1:145-158, 1998.
- 6
-
P. Giguère, G. Dumas and J. Lemay.
Gurney flap scaling for optimum lift-to-drag ratio.
AIAA Journal, 35(12):1888-1890, 1997.
- 7
-
D.W. Bechert, R. Meyer and W. Hage.
Drag reduction of airfoils with miniflaps. Can we learn from
dragonflies?
AIAA Paper 2000-2315, 2000.
- 8
-
P. Sauvage.
Étude Expérimentale et Numérique des Écoulements
potentiels et visqueux dans le Voisinage d'un Bord de Fuite Épais
Chambré.
PhD thesis, L'École Nationale Supérieure de l'Aeronautique et
de l'Espace, 1998.
- 9
-
E.A. Anderson and A.A. Szewczyk.
Effects of a splitter plate on the near wake of a circular cylinder
in 2- and 3-dimensional flow configurations.
Experiments in Fluids, 23:161-174, 1997.
- 10
-
T. Rung and F. Thiele.
Computational modelling of complex boundary-layer flows.
In 9th Int. Symp. on Transport Phenomena in Thermal-Fluid
Engineering, Singapore, 1996.
- 11
-
M. Schatz.
Numerische Simulation der Beeinflussung instationärer
Strömungsablösung durch frei bewegliche Rückstromklappen auf
Tragflügeln.
PhD thesis, Berlin University of Technology, Mensch & Buch Verlag,
Berlin, 2003.
- 12
-
P.R. Spalart, M. Shur, M. Strelets and A. Travin.
Detached-eddy simulation of an airfoil at high angle of attack.
In Engineering Turbulence Modelling and Experiments - 4.
Elsevier, Amsterdam, 1999.
- 13
-
M. Strelets.
Detached-eddy simulation of massively separated flows.
AIAA Paper 2001-0879, 2001.
- 14
-
U. Bunge, C. Mockett and F. Thiele.
Calibration of different models in the context of Detached Eddy
Simulation.
In AG STAB, Mitteilungen. DGLR, Göttingen, 2003.
- 15
-
S. Schmidt and F. Thiele.
Detached-Eddy Simulation of Flow around A-Airfoil.
Journal of Flow, Turbulence and Combustion, 71:261-278, 2003.
- 16
-
K.H. Horstmann and A. Quast.
Widerstandsverminderung durch Blasturbulatoren.
Technical report, DFVLR-FB 81-33, 1981.
- 17
-
A. Krumbein.
On modeling of transitional flow and its application on a high lift
multi-element airfoil configuration.
AIAA Paper 2003-0724, 2003.
- 18
-
R.K.J. Meyer.
Experimentelle Untersuchungen von Rückstromklappen auf
Tragflügeln zur Beeinflussung von Strömungsablösung.
PhD thesis, Berlin, University of Technology, 2000.
- 19
-
P.R. Spalart.
Young-person's guide to detached-eddy simulation grids.
CR-2001-211032, NASA, 2001.
- 20
-
M. Schatz, B. Günther and F. Thiele.
Modellierung und Analyse von Hochauftriebskonfigurationen mit
Strömungsbeeinflussung.
Abschlussbericht des SFB557, Technische Universität Berlin, 2004.
- 21
-
J. Zerihan and X. Zhang.
Aerodynamics of Gurney flaps on a wing in ground effect.
AIAA Journal, 39(5):772-780, 2001.
- 22
-
O. Brodersen, M. Rakowitz, S. Amant, P. Larrieu, D. Destarac and M. Sutcliffe.
Airbus, ONERA and DLR results from the 2nd AIAA drag
prediction workshop.
AIAA Paper 2004-0391, 2004.
- 23
-
J. Jeong and F. Hussain.
On the identification of a vortex.
J. Fluid. Mech., 285:69-94, 1995.
- 24
-
X. Zhang and J. Zerihan.
Turbulent wake behind a single element wing in ground effect.
In Proc. 10th International Symposium on Applications of Laser
Techniques to Fluid Mechanics, Lisboa, Portugal, 2000.
- 25
-
M. Myose, M. Papadakis and I. Heron.
Gurney flap experiments on airfoils, wings and reflection plane
model.
Journal of Aircraft, 35(2), 1998.
- 26
-
D.T. Yen, C.P. van Dam, R.L. Smith and S.D. Collins.
Active load control for wind turbine blades using MEM translational
tabs.
AIAA Paper 2001-0031, 2001.
- 27
-
H.T. Lee and I.M. Kroo.
Computational Investigation of Wings with Miniature Trailing Edge
Control Surfaces.
AIAA Paper 2004-2693, 2004.
Markus Schatz
2004-07-08