-
1
-
-
0018017722
-
Design of subsonic airfoils for high lift
-
R.H. Liebeck. Design of subsonic airfoils for high lift. Journal of Aircraft, 15(9), 1978.
-
(1978)
Journal of Aircraft
, vol.15
, Issue.9
-
-
Liebeck, R.H.1
-
2
-
-
0032084035
-
Numerical investigation of an airfoil with a Gurney flap
-
C.S. Jang, J.C. Ross, and R.M. Cummings. Numerical investigation of an airfoil with a Gurney flap. Aircraft Design, 1, 1998.
-
(1998)
Aircraft Design
, vol.1
-
-
Jang, C.S.1
Ross, J.C.2
Cummings, R.M.3
-
3
-
-
0033894883
-
Aerodynamics of Gurney flaps on a single-element high-lift wing
-
D. Jeffrey and X. Zhang. Aerodynamics of Gurney flaps on a single-element high-lift wing. Journal of Aircraft, 37(2), 2000.
-
(2000)
Journal of Aircraft
, vol.37
, Issue.2
-
-
Jeffrey, D.1
Zhang, X.2
-
5
-
-
0032149275
-
Navier-Stokes analysis of lift-enhancing tabs on multi-element airfoils
-
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.
-
(1998)
Aircraft Design
, vol.1
, pp. 145-158
-
-
Carrannanto, P.G.1
Storms, B.L.2
Ross, J.C.3
Cummings, R.M.4
-
6
-
-
0000445428
-
Gurney flap scaling for optimum lift-to-drag ratio
-
P. Giguère, G. Dumas, and J. Lemay. Gurney flap scaling for optimum lift-to-drag ratio. AIAA Journal, 35(12):1888-1890, 1997.
-
(1997)
AIAA Journal
, vol.35
, Issue.12
, pp. 1888-1890
-
-
Giguère, P.1
Dumas, G.2
Lemay, J.3
-
9
-
-
0000001779
-
Effects of a splitter plate on the near wake of a circular cylinder in 2- and 3-dimensional flow configurations
-
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.
-
(1997)
Experiments In Fluids
, vol.23
, pp. 161-174
-
-
Anderson, E.A.1
Szewczyk, A.A.2
-
12
-
-
0000786779
-
Detached-eddy simulation of an airfoil at high angle of attack
-
Elsevier, Amsterdam
-
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.
-
(1999)
Engineering Turbulence Modelling and Experiments - 4
-
-
Spalart, P.R.1
Shur, M.2
Strelets, M.3
Travin, A.4
-
13
-
-
0242432958
-
Detached-eddy simulation of massively separated flows
-
M. Strelets. Detached-eddy simulation of massively separated flows. AIAA Paper 2001-0879, 2001.
-
(2001)
AIAA Paper 2001-0879
-
-
Strelets, M.1
-
14
-
-
34047209875
-
Calibration of different models in the context of Detached Eddy Simulation
-
DGLR, Göttingen
-
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.
-
(2003)
AG STAB, Mitteilungen
-
-
Bunge, U.1
Mockett, C.2
Thiele, F.3
-
21
-
-
0035337132
-
Aerodynamics of Gurney flaps on a wing in ground effect
-
J. Zerihan and X. Zhang. Aerodynamics of Gurney flaps on a wing in ground effect. AIAA Journal, 39(5):772-780, 2001.
-
(2001)
AIAA Journal
, vol.39
, Issue.5
, pp. 772-780
-
-
Zerihan, J.1
Zhang, X.2
-
22
-
-
2942705981
-
-
AIAA Paper 2004-0391
-
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.
-
(2004)
Airbus, ONERA, and DLR Results From the 2nd AIAA Drag Prediction Workshop
-
-
Brodersen, O.1
Rakowitz, M.2
Amant, S.3
Larrieu, P.4
Destarac, D.5
Sutcliffe, M.6
-
23
-
-
0029252670
-
On the identification of a vortex
-
J. Jeong and F. Hussain. On the identification of a vortex. J. Fluid. Mech., 285:69-94, 1995.
-
(1995)
J. Fluid. Mech
, vol.285
, pp. 69-94
-
-
Jeong, J.1
Hussain, F.2
-
25
-
-
0032024953
-
Gurney flap experiments on airfoils, wings and reflection plane model
-
M. Myose, M. Papadakis, and I. Heron. Gurney flap experiments on airfoils, wings and reflection plane model. Journal of Aircraft, 35(2), 1998.
-
(1998)
Journal of Aircraft
, vol.35
, Issue.2
-
-
Myose, M.1
Papadakis, M.2
Heron, I.3
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