-
2
-
-
0004053853
-
-
AIAA Paper No. 98-0210
-
Donovan, J. F., Krai, L. D., and Cary, A. W., 1998, "Active Flow Control Applied to an Airfoil", AIAA Paper No. 98-0210.
-
(1998)
Active Flow Control Applied to an Airfoil
-
-
Donovan, J.F.1
Krai, L.D.2
Cary, A.W.3
-
3
-
-
0025958292
-
Separation Control: Review
-
Gad-el-Hak, M. and Bushnell, D., 1991, "Separation Control: Review", ASME Journal of Fluids Engineering, Vol. 113, pp. 5-30.
-
(1991)
ASME Journal of Fluids Engineering
, vol.113
, pp. 5-30
-
-
Gad-el-Hak, M.1
Bushnell, D.2
-
4
-
-
0142195049
-
-
Ph.D. Dissertation, Texas A&M University, Texas
-
Gilarranz, J. L., 2001, "Development of High-Power, Compact Synthetic Jet Actuators for Flow Separation Control, Ph.D. Dissertation, Texas A&M University, Texas.
-
(2001)
Development of High-Power, Compact Synthetic Jet Actuators for Flow Separation Control
-
-
Gilarranz, J.L.1
-
6
-
-
84894341899
-
Compact, High-Power Synthetic Jets for Flow Separation Control
-
Thessaloniki, Greece
-
Gilarranz, J. L., and Rediniotis, O.K., 2001b, "Compact, High-Power Synthetic Jets for Flow Separation Control, Proceedings of the Sixth National Congress on Mechanics, Thessaloniki, Greece, pp. 371-378.
-
(2001)
Proceedings of the Sixth National Congress on Mechanics
, pp. 371-378
-
-
Gilarranz, J.L.1
Rediniotis, O.K.2
-
8
-
-
2942723078
-
Separation Control By Periodic Addition of Momentum with Particular Emphasis on Dynamic Stall
-
Paper T3-4, American Helicopter Society
-
Greenblatt, D., Darabi, A., Nishri, B., and Wygnanski, L, 1998, "Separation Control By Periodic Addition of Momentum with Particular Emphasis on Dynamic Stall, " Proceedings Heli Japan 98, Paper T3-4, American Helicopter Society.
-
(1998)
Proceedings Heli Japan 98
-
-
Greenblatt, D.1
Darabi, A.2
Nishri, B.3
Wygnanski, L.4
-
11
-
-
77957128670
-
-
AIAA Paper No. 2001-0733
-
He, Y., Gary, A. W. and Peters, D. A., 2001, "Parametric and Dynamic Modeling for Synthetic Jet Control of a Post-Stall Airfoil", AIAA Paper No. 2001-0733.
-
(2001)
Parametric and Dynamic Modeling for Synthetic Jet Control of a Post-Stall Airfoil
-
-
He, Y.1
Gary, A.W.2
Peters, D.A.3
-
13
-
-
0013393142
-
-
AIAA Paper No. 2000-2401
-
Honohan, A. M., Amitay, M., and Glezer, A., 2000, "Aerodynamic Control Using Synthetic Jets", AIAA Paper No. 2000-2401.
-
(2000)
Aerodynamic Control Using Synthetic Jets
-
-
Honohan, A.M.1
Amitay, M.2
Glezer, A.3
-
14
-
-
0013389127
-
-
AIAA Paper No. 97-1824
-
Krai, L. D., Donovan, J. F., Cain, A. B. and Cary, A. W., 1997, "Numerical Simulation of Synthetic Jet Actuators", AIAA Paper No. 97-1824.
-
(1997)
Numerical Simulation of Synthetic Jet Actuators
-
-
Krai, L.D.1
Donovan, J.F.2
Cain, A.B.3
Cary, A.W.4
-
18
-
-
85040853188
-
-
Wiley, New York
-
Rae, W., and Pope, A., 1984, "Low Speed Wind Tunnel Testing", Wiley, New York, pp. 199-208, 362-424.
-
(1984)
Low Speed Wind Tunnel Testing
-
-
Rae, W.1
Pope, A.2
-
19
-
-
4243641761
-
-
AIAA Paper 2000-0407
-
Rao, P. Gilarranz, J. L., Ko, J. Strganac, T. and Rediniotis, O. K., 2000, "Flow Separation Control Via Synthetic Jet Actuation", AIAA Paper 2000-0407.
-
(2000)
Flow Separation Control Via Synthetic Jet Actuation
-
-
Rao, P.1
Gilarranz, J.L.2
Ko, J.3
Strganac, T.4
Rediniotis, O.K.5
-
20
-
-
0030820770
-
Coupled Fluid-Structural Characteristics of Actuators for Flow Control
-
Rathnasingham, R. and Breuer, K. 1997, "Coupled Fluid-Structural Characteristics of Actuators for Flow Control, " AIAA Journal, Vol. 35, pp. 832-837.
-
(1997)
AIAA Journal
, vol.35
, pp. 832-837
-
-
Rathnasingham, R.1
Breuer, K.2
-
21
-
-
0033197305
-
Oscillatory Control of Separation at High Reynolds Numbers
-
Seifert, A., and Pack, L., 1999a, "Oscillatory Control of Separation at High Reynolds Numbers", AIAA Journal, Vol. 37, pp. 1062-1071.
-
(1999)
AIAA Journal
, vol.37
, pp. 1062-1071
-
-
Seifert, A.1
Pack, L.2
-
23
-
-
35649022117
-
-
AIAA Paper No. 2000-2542
-
Seifert, A., and Pack, L., 2000, "Separation Control at Flight Reynolds Numbers: Lessons Learned and Future Directions", AIAA Paper No. 2000-2542. Seifert A., Bachat T., Koss D., Shepshelovich
-
(2000)
Separation Control at Flight Reynolds Numbers: Lessons Learned and Future Directions
-
-
Seifert, A.1
Pack, L.2
-
24
-
-
0027508904
-
Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation
-
Seifert A., Bachat T., Koss D., Shepshelovich M., Wygnanski I., 1993, "Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation", AIAA Journal, Vol. 31, pp. 2052-2060.
-
(1993)
AIAA Journal
, vol.31
, pp. 2052-2060
-
-
Seifert, A.1
Bachat, T.2
Koss, D.3
Shepshelovich, M.4
Wygnanski, I.5
-
25
-
-
0030197223
-
On the delay of Airfoil Stall by Periodic Excitation
-
Seifert, A., Darabi, A., and Wygnanski, L, 1996, "On the delay of Airfoil Stall by Periodic Excitation", Journal of Aircraft, Vol. 33, pp. 691-699.
-
(1996)
Journal of Aircraft
, vol.33
, pp. 691-699
-
-
Seifert, A.1
Darabi, A.2
Wygnanski, L.3
-
26
-
-
0000244672
-
On the Use of Piezoelectric Actuators for Airfoil Separation Control
-
Seifert A, Eliahu S, Greenblatt D, Wygnanski I, 1998, "On the Use of Piezoelectric Actuators for Airfoil Separation Control", AIAA Journal, Vol. 36, pp. 1535-1537.
-
(1998)
AIAA Journal
, vol.36
, pp. 1535-1537
-
-
Seifert, A.1
Eliahu, S.2
Greenblatt, D.3
Wygnanski, I.4
-
28
-
-
33645661580
-
-
AIAA Paper No. 99-0669
-
Smith, B. L., Trautman, M. A., and Glezer, A., 1999, "Controlled Interactions of Adjacent Synthetic Jets", AIAA Paper No. 99-0669.
-
(1999)
Controlled Interactions of Adjacent Synthetic Jets
-
-
Smith, B.L.1
Trautman, M.A.2
Glezer, A.3
-
29
-
-
84982318012
-
-
AIAA Paper No. 98-0209
-
Smith, D., Amitay M., Kibens V., Parekh D. and Glezer A., 1998, "Modifications of Lifting Body Aerodynamics Using Synthetic Jet Actuators, " AIAA Paper No. 98-0209.
-
(1998)
Modifications of Lifting Body Aerodynamics Using Synthetic Jet Actuators
-
-
Smith, D.1
Amitay, M.2
Kibens, V.3
Parekh, D.4
Glezer, A.5
-
30
-
-
20444461177
-
-
NACA R. M. A50J09, NACA, Washington D. C
-
Summers, J. L., and Page, W. A., 1950, Lift and Moment Characteristics at Subsonic Mach Numbers of Four 10-Percent-Thick Airfoil Sections of Varying Trailing-Edge Thickness, NACA R. M. A50J09, NACA, Washington D.C.
-
(1950)
Lift and Moment Characteristics at Subsonic Mach Numbers of Four 10-Percent-Thick Airfoil Sections of Varying Trailing-Edge Thickness
-
-
Summers, J.L.1
Page, W.A.2
-
31
-
-
3242855741
-
-
M.S. Thesis, University of the Witwatersrand, Johannesburg, South Africa
-
Traub, L. W., 1992, "A Subsonic Wind-Tunnel Investigation of the Effect of Sharp Edged Sheared Tips on a Moderate Aspect Ratio Flat Plate Wing", M.S. Thesis, University of the Witwatersrand, Johannesburg, South Africa.
-
(1992)
A Subsonic Wind-Tunnel Investigation of the Effect of Sharp Edged Sheared Tips on a Moderate Aspect Ratio Flat Plate Wing
-
-
Traub, L.W.1
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