Reynolds number and wind tunnel wall effects on the flow field around a generic UHBR engine high-lift configuration    2020
J Ullah, A Prachař, M Šmíd, A Seifert, V Soudakov, T Lutz, E Krämer    
CEAS Aeronautical Journal 11 (4), 1009-1023    
   
Device and method for creating a distribution of unsteady suction    2020
A Seifert, N Shay, A Yaniv, O Drori    
US Patent App. 16/454,077    
   
The Oscillatory Suction Actuator: Fundamentals, Interactions and Efficiency    2020
B Mizrahi, A Seifert    
AIAA AVIATION 2020 FORUM, 2941    
   
Suction and pulsed blowing for control of local wing-engine-slat-cut out flow separation: The INAFLOWT Project    2020
S Monat, M Posti, B Mizrahi, A Yaniv, A Seifert, O Drori    
AIAA AVIATION 2020 FORUM, 2953    
   
A Comparison Between Oscillatory and Steady Suction for Airfoil Separation Control    2019
A Seifert, B Mizrahi    
APS, P26. 003    
   
On the Interaction of Unsteady Suction and Turbulent Flat Plate Boundary Layer    2019
B Mizrahi, A Seifert    
APS, P26. 002    
   
The Unsteady Suction Actuator    2019
N Shay, B Mizrahi, O Drori, A Yaniv, A Seifert    
APS, P26. 001    
   
Suction and Oscillatory Blowing Flow Control of External Store Support System Flight Hardware    2019
David Schatzman, Jacob Wilson, CCDC AvMC ADD; Ofek Drori, Avraham Seifert, Tel Aviv University    
The Vertical Flight Society, 75th Annual Forum    
   
Data-driven modeling of pitching and plunging tandem wings in hovering flight    2019
V Troshin, A Seifert    
Experiments in Fluids 60 (3), 39    
   
Active flow control virtual maneuvering system applied to conventional airfoil    2019
D Dolgopyat, A Seifert    
AIAA Journal 57 (1), 72-89    
   
Wing-tip flow separation control using localized steady suction    2018
M Lagutin, I Detenis, A Seifert    
Bulletin of the American Physical Society 63    
   
Capability of RANS Simulations to Reproduce Flat Plate Boundary Layer Interaction with Suction and Oscillatory Blowing    2018
J Ullah, N Shay, M Possti, A Seifert, T Lutz, E Krämer    
Symposium der Deutsche Gesellschaft für Luft-und Raumfahrt, 630-640    
   
The Development of ¼ Model Test Capabilities for Heavy Road Vehicles Drag Reduction Studies    2018
T Domb, A Seifert    
Third International Conference in numerical and experimental aerodynamics of …    
   
Boundary layer separation control: Experimental perspective and modeling outlook    2018
A Seifert, A Yaniv    
Annu. Rev. Fluid Mech 50    
   
Active Buffet Control on Wing Trailing Edge    2018
M Nichols, F Sartor, J Dandois, JEJ Maseland, M Minervino, A Ryzhov, ...    
   
Modeling of a pitching and plunging airfoil using experimental flow field and load measurements    2018
V Troshin, A Seifert    
Experiments in Fluids 59 (1), 6    
   
Large-eddy simulation-based characterization of suction and oscillatory blowing fluidic actuator    2017
J Kim, P Moin, A Seifert    
AIAA Journal 55 (8), 2566-2579    
   
Synchronization of fluidic actuators    2017
A Seifert, I Dayan, T Shtendel    
US Patent 9,718,538    
   
Characterization of SaOB actuators interacting with flat plate boundary layers    2017
J Wilson, DM Schatzman, A Seifert, E Arad, L Marom, N Shay, V Palei    
55th AIAA Aerospace Sciences Meeting, 1691    
   
Active flow control insight gained from a modified integral boundary layer equation    2016
A Seifert    
APS, L7. 005    
   
Measurement and Modelling of a Heaving Airfoil Flow    2016
V Troshin, A Seifert    
APS, R6. 006    
   
System and method for multiple direction control of flow    2016
A Seifert, D Dolgopyat    
US Patent App. 15/025,287    
   
Fluidic flow control applied for improved performance of Darrieus wind turbines    2016
N Morgulis, A Seifert    
Wind Energy 19 (9), 1585-1602    
   
Proper orthogonal decomposition of flow-field in non-stationary geometry    2016
V Troshin, A Seifert, D Sidilkover, G Tadmor    
Journal of Computational Physics 311, 329-337    
   
Active flow control and part-span slat interactions    2016
D Sarkorov, A Seifert, I Detinis, S Bauminger, M Steinbuch    
AIAA Journal 54 (3), 1095-1106    
   
LES-based characterization of a suction and oscillatory blowing fluidic actuator    2016
J Kim, P Moin, A Seifert    
54th AIAA Aerospace Sciences Meeting, 0572    
   
Stereo PIV measurements of Suction and Pulsed Blowing Interaction with a Laminar Boundary Layer    2016
L Marom, N Shay, A Seifert    
18th International Symposium on the Application of Laser and Imaging …    
   
Closed-Loop Flow Control of the Oscillations of a Free-Suspended Cylinder at Low Reynolds Numbers    2016
AC Hillier, O Friedland, A Seifert    
8th AIAA Flow Control Conference, 4083    
   
On the Response of a Separating Turbulent Boundary Layer to High Amplitude Excitation    2016
V Palei, A Seifert    
Progress in Wall Turbulence 2, 307-316    
   
From lab to full scale Active Flow Control drag reduction: How to bridge the gap?    2015
A Seifert, T Shtendel, D Dolgopyat    
Journal of Wind Engineering and Industrial Aerodynamics 147, 262-272    
   
Methods and apparatus for reduction of aerodynamic drag    2015
A Seifert, V Palei    
US Patent 9,193,398    
   
Interaction of suction and pulsed blowing with a laminar boundary layer    2015
A Seifert, L Marom    
APS, L15. 012    
   
The ultimate flow controlled wind turbine blade airfoil    2015
A Seifert, D Dolgopyat, O Friedland, L Shig    
APS, KP1. 007    
   
Flow Control Applied to the Rounded Front Edges of a Square Prism    2015
AS G. Lubinsky    
International Journal of Flow Control 7 (1-2), 1-18    
   
Trailing edge noise reduction of wind turbine blades by active flow control    2015
A Wolf, T Lutz, W Würz, E Krämer, O Stalnov, A Seifert    
Wind Energy 18 (5), 909-923    
   
Suction and Pulsed Blowing Interaction with a Laminar Boundary Layer    2015
L Marom, V Palei, A Seifert    
55th ISR Aero Conf    
   
Evaluation criteria and performance comparison of actuators    2015
A Seifert    
Instability and Control of Massively Separated Flows: Proceedings of the …    
   
Suction and oscillatory blowing interaction with boundary layers    2015
DM Schatzman, J Wilson, L Maron, V Palei, A Seifert, E Arad    
53rd AIAA Aerospace Sciences Meeting, 0808    
   
Suction and Oscillatory Blowing Applied to the Rounded Front Edges of a Square Prism    2015
G Lubinsky, A Seifert    
Instability and Control of Massively Separated Flows, 157-162    
   
Oscillatory vorticity generator and applications thereof    2014
A Seifert, O Stalnov, I Fono, I Dayan, V Troshin, MH Avnaim, V Palei    
US Patent 8,876,064    
   
Drag-reduction mechanisms of suction-and-oscillatory-blowing flow control    2014
D Schatzman, J Wilson, E Arad, A Seifert, T Shtendel    
AIAA Journal 52 (11), 2491-2505    
   
On the Efficiency of Fluidic Oscillators for Aerofoil Performance Recovery    2014
D Sarkorov, A Seifert    
APS, A30. 001    
   
Flow Control Applied to the Front Rounded Edge of a Bluff Body    2014
G Lubinsky, A Seifert    
International Journal of Flow Control 6 (1), 21-42    
   
Characterization of the suction and oscillatory blowing actuator in still air    2014
V Troshin, V Palei, T Shtendel, A Seifert    
Proceedings of the 54th Israel Annual Conference on Aerospace Sciences, Tel …    
   
Three-dimensional Aspects of bluff-body drag reduction by active flow control    2014
T Shtendel, A Seifert    
Int. J. Heat and Flow 45, 109-127    
   
Three-dimensional aspects of cylinder drag reduction by suction and oscillatory blowing    2014
T Shtendel, A Seifert    
International journal of heat and fluid flow 45, 109-127    
   
Drag-Reduction Mechanisms of Suction-and-Oscillatory-Blowing Flow Control    2014
A Seifert, T Shtendel, D Schatzman, J Wilson, E Arad    
   
Active Flow Control Maneuvering System    2014
D Dolgopyat, A Seifert    
54th Israel Annual Conference on Aerospace Sciences    
   
WIND LOADS AND CONTROL OF FLEXIBLE STRUC-TURES EMBEDDED IN A TURBULENT BOUNDARY LAYER: MECHANICAL CONTROL    2014
O Friedland, V Troshin, A Seifert    
21st Int. Congr. Sound Vib    
   
Evaluation criteria and performance comparison of actuators for bluff-body flow control    2014
A Seifert    
32nd AIAA Applied Aerodynamics Conference, 2400    
   
Methods and apparatus for reduction of aerodynamic drag    2013
A Seifert, V Palei    
US Patent 8,616,615    
   
Efficiency of Flow Control Actuators    2013
A Seifert    
APS, M25. 004    
   
Suction and pulsed-blowing flow control applied to an axisymmetric body    2013
J Wilson, D Schatzman, E Arad, A Seifert, T Shtendel    
AIAA journal 51 (10), 2432-2446    
   
Empirical model for the evolution of a vortex-pair introduced into a boundary layer    2013
T Yehoshua, A Seifert    
   
Phase-locked 3D3C-MRV measurements in a bi-stable fluidic oscillator    2013
F Wassermann, D Hecker, B Jung, M Markl, A Seifert, S Grundmann    
Experiments in fluids 54 (3), 1487    
   
Suction and Pulsed-Blowing Flow Control Applied to an Axisymmetric Body    2013
A Seifert, T Shtendel, D Schatzman, J Wilson, E Arad    
   
Flow Physics of Drag Reduction Mechanism using Suction and Pulsed Blowing    2013
D Schatzman, J Wilson, E Arad, A Seifert, T Shtendel    
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and …    
   
Performance recovery of a thick turbulent airfoil using a distributed closed-loop flow control system    2013
V Troshin, A Seifert    
Experiments in fluids 54 (1), 1443    
   
On the generation of yawing moment using active flow control    2012
S David, A Seifert    
International journal of heat and fluid flow 38, 72-81    
   
Erratum to: Closed-loop bluff-body wake stabilization via fluidic excitation    2012
O Stalnov, I Fono, A Seifert    
Theoretical and Computational Fluid Dynamics 26 (5), 483    
   
Active Separation Control Applied to an Axis-symmetric Body    2012
J Wilson, D Schatzman, E Arad, T Shtendel, A Seifert    
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …    
   
On the Evolution of Amplitude Modulated Excitation in Still Air.    2011
T Yehoshua, A Seifert    
International Journal of Flow Control 3    
   
Closed-loop bluff-body wake stabilization via fluidic excitation    2011
O Stalnov, I Fono, A Seifert    
Theoretical and Computational Fluid Dynamics 25 (1-4), 209-219    
   
On the Application of Active Flow Control to Wind Turbines    2011
A Seifert, O Stalnov, V Troshin, MH Avnaim    
Fluids Engineering Division Summer Meeting 44403, 3057-3064    
   
Evaluation of active flow control applied to wind turbine blade section    2010
O Stalnov, A Kribus, A Seifert    
Journal of Renewable and Sustainable Energy 2 (6), 063101    
   
Parameter study of simplified dragonfly airfoil geometry at Reynolds number of 6000    2010
DE Levy, A Seifert    
Journal of theoretical biology 266 (4), 691-702    
   
Heavy trucks fuel savings using the SaOB actuator    2010
A Seifert, I Dayan, C Horrell, J Grossmann, A Smith    
International Conference on Engineering Conferences International, 377-390    
   
Roll Control via Active Flow Control: From Concept to Flight    2010
A Seifert, S David, I Fono, O Stalnov, I Dayan    
Journal of Aircraft 47 (3), 864-874    
   
External and Turbomachinery Flow Control Working Group    2010
R Wallace, B McKeon, S Obcid, J Dannenhoffer, H Hodson, A Shahabi, ...    
   
Impact of Suction on Boundary-Layer and Noise Emission of Wind Turbine Airfoils    2010
A Wolf, O Stalnov, T Lutz, W Würz, A Seifert, E Krämer    
German Wind Energy Conference    
   
On amplitude scaling of active separation control    2010
O Stalnov, A Seifert    
Active Flow Control II, 63-80    
   
Nonlinear electrokinetic phenomena around nearly insulated sharp tips in microflows    2009
Y Eckstein, G Yossifon, A Seifert, T Miloh    
Journal of colloid and interface science 338 (1), 243-249    
   
Simplified dragonfly airfoil aerodynamics at Reynolds numbers below 8000    2009
DE Levy, A Seifert    
Physics of fluids 21 (7), 071901    
   
Fixed wing airfoil applications    2009
A Seifert, C Tilmann    
Fundamentals and Applications of Modern Flow Control 231, 231-257    
   
Large trucks drag reduction using active flow control    2009
A Seifert, O Stalnov, D Sperber, G Arwatz, V Palei, S David, I Dayan, ...    
The Aerodynamics of Heavy Vehicles II: Trucks, Buses, and Trains, 115-133    
   
APPARATUS AND METHOD FOR OSCILLATING FLUID JETS    2008
G ARWATZ, I FONO, A SEIFERT    
WO Patent WO/2008/135,967    
   
Suction and oscillatory blowing actuator modeling and validation    2008
G Arwatz, I Fono, A Seifert    
AIAA journal 46 (5), 1107-1117    
   
Large trucks drag reduction using active flow control    2008
A Seifert, O Stalnov, D Sperber, G Arwatz, V Palei, S David, I Dayan, ...    
46th AIAA Aerospace Sciences Meeting and Exhibit, 743    
   
Heavy trucks drag reduction by active flow control    2008
A Seifert, O Stalnov, D Sperber, A Arwatz, V Palei, S David, I Dayan, ...    
AIAA paper 743    
   
Collaborative studies on flow separation control    2008
WL Siauw, JP Bonnet, J Tensi, A Seifert, O Stalnov, V Kumar, F Alvi, ...    
IUTAM Symposium on Flow Control and MEMS, 157-166    
   
Suction and oscillatory blowing actuator    2008
G Arwatz, I Fono, A Seifert    
IUTAM Symposium on Flow Control and MEMS, 33-44    
   
Computational and Experimental Study of Circular Cylinder Flow Control    2008
E Arad, D Sperber, A Seifert    
38th Fluid Dynamics Conference and Exhibit, 4379    
   
High-performance wind turbines using active flow control    2008
O Stalnov, A Kribus, A Seifert    
48th Israel Annual Conference on Aerospace Sciences    
   
Effects of periodic excitation on the flow around a D-shaped cylinder at low Reynolds numbers    2007
V Palei, A Seifert    
Flow, turbulence and combustion 78 (3-4), 409-428    
   
Generic transport aft-body drag reduction using active flow control    2007
E Ben-Hamou, E Arad, A Seifert    
Flow, turbulence and combustion 78 (3-4), 365    
   
Maneuvering aspects and 3D effects of active airfoil flow control    2007
I Timor, E Ben-Hamou, Y Guy, A Seifert    
Flow, turbulence and combustion 78 (3-4), 429-443    
   
Active control of a circular cylinder flow at transitional Reynolds numbers    2007
A Naim, D Greenblatt, A Seifert, I Wygnanski    
Flow, turbulence and combustion 78 (3), 383-407    
   
Experimental estimation of a D-shaped cylinder wake using body-mounted sensors    2007
O Stalnov, V Palei, I Fono, K Cohen, A Seifert    
Experiments in fluids 42 (4), 531-542    
   
On the evolution of localized disturbances and their spanwise interactions leading to breakdown    2007
A Seifert    
   
On the receptivity of a boundary layer to high-amplitude excitation    2007
T Yehoshua, A Seifert    
37th AIAA Fluid Dynamics Conference and Exhibit, 3994    
   
Closed-loop active flow control systems: actuators    2007
A Seifert    
Active Flow Control, 85-102    
   
Technique for backward particle tracking in a flow field    2006
A Nahum, A Seifert    
Physical Review E 74 (1), 016701    
   
Boundary condition effects on the evolution of a train of vortex pairs in still air    2006
T Yehoshua, A Seifert    
The Aeronautical Journal 110 (1109), 397-417    
   
On the application of confined twin-jet instability to micro-mixing enhancement    2006
A Nahum, A Seifert    
Physics of Fluids 18 (6), 064107    
   
Method and mechanism for producing suction and periodic excitation flow    2006
A Seifert, S Pastuer    
US Patent 7,055,541    
   
Active boundary layer tripping using oscillatory vorticity generator    2006
T Yehoshua, A Seifert    
Aerospace Science and Technology 10 (3), 175-180    
   
Method and mechanism for producing suction and periodic flow    2006
A Seifert, S Pastuer    
US Patent, 0048829-A1    
   
Control and identification of turbulent boundary layer separation    2006
A Seifert, LTP Melton    
IUTAM Symposium on One Hundred Years of Boundary Layer Research, 199-208    
   
Active control of separation from the flap of a supercritical airfoil    2006
LTP Melton, CS Yao, A Seifert    
AIAA journal 44 (1), 34-41    
   
Active control of flow separation from supercritical airfoil leading-edge flap shoulder    2005
LTP Melton, NW Schaeffler, CS Yao, A Seifert    
Journal of Aircraft 42 (5), 1142-1149    
   
Experimental validation of sensor placement for control of a    2005
VP Stalnov, I Fono, K Cohen, A Seifert    
D" shaped cylinder wake", presented at the 35th AIAA Fluid Dynamics …    
   
Delta wing stall and roll control using segmented piezoelectric fluidic actuators    2005
S Margalit, D Greenblatt, A Seifert, I Wygnanski    
Journal of aircraft 42 (3), 698-709    
   
Multiple Actuators Flow Control over a Glauert-Goldschmied type Airfoil at Low Reynolds Numbers    2005
J Yom-Tov, A Seifert    
35th AIAA Fluid Dynamics Conference and Exhibit, 5389    
   
Experimental validation of sensor placement for control of a D-shaped cylinder wake    2005
O Stalnov, V Palei, I Fono, K Cohen, A Seifert    
35th AIAA Fluid Dynamics Conference and Exhibit, 5260    
   
Effects of elevated free-stream turbulence on actively controlled separation bubble    2004
E Halfon, B Nishri, A Seifert, I Wygnanski    
J. Fluids Eng. 126 (6), 1015-1024    
   
Active separation control: an overview of Reynolds and Mach numbers effects    2004
A Seifert, D Greenblatt, IJ Wygnanski    
Aerospace Science and technology 8 (7), 569-582    
   
Issues in active flow control: theory, control, simulation, and experiment    2004
S Scott Collis, RD Joslin, A Seifert, V Theofilis    
Progress in Aerospace Sciences 40 (4), 237-289    
   
Aerial vehicle controlled and propelled by oscillatory momentum generators and method of flying a vehicle    2004
A Seifert, D Greenblatt, I Wygnanski    
US Patent 6,751,530    
   
Sensor Placement for Closed-Loop Flow Control of a" D" Shaped Cylinder Wake    2004
K Cohen, S Siegel, M Luchtenburg, T McLaughlin, A Seifert    
2nd AIAA flow control conference, 2523    
   
Use of multiple actuators for jet vectoring    2004
LT Pack-Melton, A Seifert    
Journal of propulsion and power 20 (3), 572-575    
   
Application of excitation from multiple locations on a simplified high-lift system    2004
L Pack Melton, CS Yao, A Seifert    
2nd AIAA Flow Control Conference, 2324    
   
Exploiting the Confined Twin-Jet Instability for Micro Mixing Enhancement    2004
A Nahum, A Seifert    
ASME International Mechanical Engineering Congress and Exposition 47098, 237-242    
   
Effects of sweep on the dynamics of active separation control    2003
LG Pack, A Seifert    
The Aeronautical Journal 107 (1076), 617-629    
   
Cellulase preparation comprising an endoglucanase enzyme    2003
G Rasmussen, J Mikkelsen, M Schulein, S Patkar, F Hagen, C Hjort, ...    
US Patent App. 10/138,870    
   
Boundary condition effects on oscillatory momentum generator    2003
T Yehoshua, A Seifert    
33rd AIAA Fluid Dynamics Conference and Exhibit, 3710    
   
Effects of sweep on active separation control at high Reynolds numbers    2003
A Seifert, LTG Pack    
Journal of Aircraft 40 (1), 120-126    
   
Compressibility and excitation location effects on high Reynolds numbers active separation control    2003
A Seifert, LTG Pack    
Journal of Aircraft 40 (1), 110-119    
   
Rotation of a rectangular jet by periodic excitation    2003
E Avihar, N Shemesh, A Seifert, LG Pack    
Journal of aircraft 40 (1), 217-219    
   
Closed-loop vectoring control of a turbulent jet using periodic excitation    2003
D Rapoport, I Fono, K Cohen, A Seifert    
Journal of propulsion and power 19 (4), 646-654    
   
Mini UAV's: Can Active Flow Control Do It All?    2002
A Seifert    
TEL-AVIV UNIV (ISRAEL) DEPT OF FLUID MECHANICS AND HEAT TRANSFER    
   
Flow Control Experiments, Simulation and Modeling Approaches    2002
A Seifert, R Joslin, V Theofilis    
1st Flow Control Conference, 3277    
   
Effects of elevated free-stream turbulence on active control of a transitional separation bubble    2002
E Halfon, B Nishri, A Seifert, I Wygnanski    
1st Flow Control Conference, 3169    
   
Effects of elevated free-stream turbulence on active control of a separation bubble    2002
A Seifert, B Nishri, I Wygnanski, E Halfon    
1 st AIAA Flow Control Conference, Saint Louis, MO    
   
Active control of cylinder flow with and without a splitter plate using piezoelectric actuators    2002
A Seifert, A Naim, I Wygnanski    
1 st AIAA Flow Control Conference, Saint Louis, MO    
   
Active control of a transitional separation bubble at low Reynolds number and elevated free-stream turbulence    2002
B Nishri, A Seifert, I Wygnanski    
Minnowbrook III: 2000 Workshop on Boundary Layer Transition and Unsteady …    
   
Active flow separation control on wall-mounted hump at high Reynolds numbers    2002
A Seifert, LG Pack    
AIAA journal 40 (7), 1363-1372    
   
Active control of flow separation from the slat shoulder of a supercritical airfoil    2002
LG Pack, NW Schaeffler, CS Yao, A Seifert    
   
Airfoil with dynamic stall control by oscillatory forcing    2001
I Wygnanski, D Greenblatt, A Seifert    
US Patent 6,267,331    
   
Apparatus and method for controlling the motion of a solid body or fluid stream    2001
A Seifert, I Wygnanski    
US Patent 6,250,586    
   
Periodic excitation for jet vectoring and enhanced spreading    2001
LG Pack, A Seifert    
Journal of aircraft 38 (3), 486-495    
   
Active separation control: From basic research to a simplified high-lift system    2001
A Seifert    
SAE transactions, 491-499    
   
Multiple mode actuation of a turbulent jet    2001
L Pack, A Seifert    
39th Aerospace Sciences Meeting and Exhibit, 735    
   
Closed-loop separation control using oscillatory flow excitation    2000
BG Allan, JN Juang, DL Raney, A Seifert, DE Brown    
   
Dynamics of active separation control at high Reynolds numbers    2000
LT Pack, A Seifert    
38th Aerospace Sciences Meeting and Exhibit, 409    
   
Separation control at flight Reynolds numbers-Lessons learned and future directions    2000
A Seifert, LT Pack    
Fluids 2000 Conference and Exhibit, 2542    
   
Periodic turbulent strips and calmed regions in a transitional boundary layer    1999
A Seifert, HP Hodson    
AIAA journal 37 (9), 1127-1129    
   
Oscillatory control of separation at high Reynolds numbers    1999
A Seifert, LG Pack    
AIAA journal 37 (9), 1062-1071    
   
Application of active separation control to a small unmanned air vehicle    1999
A Seifert, T Bachar, I Wygnanski, A Kariv, H Cohen, R Yoeli    
Journal of aircraft 36 (2), 474-477    
   
MEMS-based probes for velocity and pressure measurements in unsteady and turbulent flowfields    1999
LP Othon Rediniotis, Espen Johansen, T. Tsao, A. Seifert    
37th Aerospace Sciences Meeting and Exhibit. January    
   
Oscillatory excitation of unsteady compressible flows over airfoils at flight Reynolds numbers    1999
A Seifert, L Pack    
AIAA paper 925, 1999    
   
MEMS-based probes for velocity and pressure measurements in unsteady and turbulent flowfields    1999
O Rediniotis, E Johansen, T Tsao, A Seifert, L Pack    
37th Aerospace Sciences Meeting and Exhibit, 521    
   
Use of piezoelectric actuators for airfoil separation control    1998
A Seifert, S Eliahu, D Greenblatt, I Wygnanski    
AIAA journal 36 (8), 1535-1537    
   
Sweep effect on parameters governing control of separation by periodic excitation    1998
T Naveh, A Seifert, A Tumin, I Wygnanski    
Journal of aircraft 35 (3), 510-512    
   
Pressure Gradient Boundary-Layer Transition: Experiment and Linear Stability Analysis    1998
A Seifert, A Tumin    
Progress In Astronautics and Aeronautics: Single-and Multi-Phase Flows In an …    
   
Spot Calming Effect on Boundary Layer Transition (Minnowbrook 1997)    1998
A Seifert    
1997 Workshop on Boundary Layer, 99    
   
Nonlinear localized disturbances in an adverse pressure gradient boundary-layer transition- Experiment and linear stability analysis    1998
A Seifert, A Tumin    
Progress in fluid flow research: Turbulence and applied MHD, 3-13    
   
Lift enhancement using pulsed blowing at compressible flow conditions    1997
M Hites, H Nagib, B Sytsma, I Wygnanski, A Seifert, T Bachar    
APS, Ef. 08    
   
Wygnanski,“Delay of airfoil stall by periodic excitation”    1996
A Seifert, A Darabi    
Journal of Aircraft 33 (4), 691-699    
   
Delay of airfoil stall by periodic excitation    1996
A Seifert, A Darabi, I Wyganski    
Journal of aircraft 33 (4), 691-698    
   
Non-linear evolution of point-source disturbances in an adverse pressure gradient laminar boundary layer    1996
A Seifert    
IUTAM Symposium on Nonlinear Instability and Transition in Three-Dimensional …    
   
On turbulent spots in a laminar boundary layer subjected to a self-similar adverse pressure gradient    1995
A Seifert, IJ Wygnanski    
Journal of Fluid Mechanics 296, 185-209    
   
The control of separation by periodic oscillations    1994
I Wygnanski, A Seifert    
25th Plasmadynamics and Lasers Conference, 2608    
   
On the simultaneous measurements of two velocity components in the turbulent spot    1994
A Seifert, M Zilberman, I Wygnanski    
Journal of engineering mathematics 28 (1), 43-54    
   
Oscillatory blowing: a tool to delay boundary-layer separation    1993
A Seifert, T Bachar, D Koss, M Shepshelovich, I Wygnanski    
AIAA journal 31 (11), 2052-2060    
   
On the Non Linear Spanwise Interaction of Disturbances Emanating from Two Point Sources in a Blasius Boundary Layer.    1993
A Seifert, I Wygnanski    
TEL-AVIV UNIV (ISRAEL) DEPT OF FLUID MECHANICS AND HEAT TRANSFER    
   
The effects of forced oscillations on the performance of airfoils    1993
A Seifert, A Daraby, B Nishri, I Wygnanski    
3rd Shear Flow Conference, 3264    
   
Pilot Test of Low Reynolds Number DTE-Airfoil    1993
D Koss, S Bauminger, M Shepshelovich, A Seifert, I Wygnansky    
AIAA 93-0643, 31st Aerospace Sciences Meeting and Exibit    
   
On the interaction of wave trains emanating from two point sources in a Blasius boundary layer    1991
A Seifert, I Wygnanski    
bltc, 7.1-7.13    
   
On the origin and control of large coherent structures in turbulent shear flow(Final Technical Report, 15 Feb. 1989- 14 Aug.)(1990)    1991
A SEIFERT, I WYGNANSKI    
   
On the evolution of the turbulent spot in a laminar boundary layer with a favourable pressure gradient    1990
Y Katz, A Seifert, I Wygnanski    
Journal of fluid mechanics 221, 1-22    
   
On the interaction of low amplitude disturbances emanating from discrete points in a Blasius boundary layer    1990
A Seifert    
Tel Aviv University.    
   
An Experimental Evaluation of Low Reynolds Number High-Lift Airfoil with Vanishingly Small Pitching Moment    1989
A Shepshelovich, M., Koss, D., Wygnanski, I. and Seifert    
27th AIAA Aerospace Sciences Meeting 1989 (AlAA paper 89-0538)    
   
Active Flow Separation Control on a Generic UHBR Engine High-Lift Configuration by Means of Suction and Oscillatory Blowing    
J Ullah, S Monat, A Seifert, T Lutz, E Krämer    
Fundamentals of High Lift for Future Civil Aircraft, 365-384    
   
The Ultimate Flow Controlled Wind Turbine Blade Airfoil    
S Avraham, F Ori, D Danny    
Projektgruppe/Fachkreis: Transportflugzeuge einschl. Triebwerksintegration    
J Ullah, N Shay, A Seifert, T Lutz, E Krämer    
   
SIMPLIFIED OSCILLATORY BOUNDARY CONDITION FOR EFFICIENT CFD SIMULATION OF AFC EFFECT    
P Vrchota, A Prachař, P Hospodář, D Dolgopyat, A Seifert    
   
WIND LOADS AND CONTROL OF FLEXIBLE STRUC-TURES EMBEDDED IN A TURBULENT BOUNDARY LAYER: FLUIDIC CONTROL    
A Seifert, O Friedland, V Troshin    
   
Dynamic Characterization of the Suction and Oscillatory Blowing Actuator    
V Troshin, O Stalnov, T Shtendel, A Seifert