JOURNAL ARTICLES
1.
Katz, Y., Seifert,
A., and Wygnanski, I., 1990, "On the
Evolution of a Turbulent Spot in a Favorable Pressure Gradient", J. of
Fluid Mechanics, Vol. 221, pp. 1-22.
2.
Seifert, A., Bachar,
T., Koss, D., Shepshelovits, M. and Wygnanski, I.,
1993, "Oscillatory Blowing, a Tool to Delay Boundary Layer
Separation", AIAA J. Vol. 31, No. 11, pp. 2052-2060.
3.
Seifert, A.,
Zilberman, M. and Wygnanski, I., 1994,
"On the Simultaneous Measurement of Two Velocity Components in a Turbulent
Spot", J. of Engineering Mathematics, 28, pp. 43-54.
4.
Seifert, A. and
Shemer, L., 1995, “Plume Rise From a Chimney with an Elongated Exit
Cross-Section”, Atmospheric Environment, Vol. 29, No. 6, pp. 709-713.
5.
Seifert, A., and
Wygnanski, I., 1995, "On Turbulent Spots
in a Laminar Boundary Layer Subjected to a Self-Similar Adverse Pressure
Gradient”, J. Fluid Mech. 296, Aug. 10, pp. 185-209.
6.
Seifert, A., Darabi,
A. and Wygnanski, I., 1996, “Delay of Airfoil Stall by Periodic
Excitation”, J. of Aircraft. Vol. 33, No. 4, pp. 691-699.
7.
Naveh, T. Seifert,
A., Tumin, A. and Wygnanski, I., 1998, “Sweep Effect on the Parameters Governing the
Control of Separation by Periodic Excitation”, J. of Aircraft. Vol. 35,
No. 3, pp. 510-512.
8.
Seifert, A., Eliahu,
S., Greenblatt, D. and Wygnanski, I.,
1998, “Use of Piezoelectric Actuators
for Airfoil Separation Control (TN)”, AIAA J., Vol. 36, No. 8, pp.
1535-1537.
9.
Seifert, A., Bachar,
T., Wygnanski, I., Kariv, A., Cohen, H. and
Yoeli, R., “Application of Active Separation Control to a Small UAV”, J.
Aircraft, Vol. 36, No. 2, March-April 1999, pp. 474-477.
10.
Seifert, A. and Pack,
L.G., “Oscillatory Control of Separation at High Reynolds Numbers”, AIAA J.
Vol. 37, No. 9, Sep. 1999, pp. 1062-1071.
11.
Seifert, A. and
Hodson, H.P., “Periodic Turbulent Strips and Calmed Regions in a Transitional
Boundary Layer (TN)”, AIAA J., Vol. 37, No. 9, Sep. 1999, pp. 1127-1129.
12.
Pack, L.G. and
Seifert, A., “Periodic Excitation for Jet Vectoring and Enhanced Spreading”,
(AIAA paper 99-0672), J. Aircraft, May-June 2001, V38, N3, pp. 486-495.
13.
Seifert, A. and Pack,
L.G., “Oscillatory Control of Shock-induced Separation”, (AIAA paper 99-0925), J.
Aircraft, May-June 2001, V38, N3, pp. 464-472.
14.
Seifert, A., “Active
Separation Control: From Basic Research to a Simplified High-lift System”, SAE
paper 2001-01-2945., September 2001. SAE Transactions J. of Aerospace.
15.
Seifert, A. and Pack,
L.G., “Active Control of Separated Flow on a Wall-mounted “Hump” at High
Reynolds Numbers”, AIAA J., V. 40, No. 7, July, 2002, pp. 1363-1372.
(Part of AIAA paper 99-3430).
16.
Seifert, A. and Pack,
L.G., “Effects of Compressibility and Excitation Slot Location on Active
Separation Control at High Reynolds Numbers”, J. Aircraft 40, (1): pp. 110-119
Jan-Feb 2003.
17.
Seifert, A. and Pack,
L.G., “Effects of Sweep on Active Separation Control at High Reynolds Numbers”,
J. Aircraft, 40 (1): pp. 120-126 Jan-Feb 2003.
18.
Avihar, E., Shemesh,
N., Pack, L.G. and Seifert, A., “Rotation of a Rectangular Jet by Periodic
Excitation”, J. Aircraft, 40 (1):
pp. 217-219 Jan-Feb 2003.
19.
Rapoport, D., Fono, I., Cohen, K. and Seifert, A., “Closed-loop Vectoring
Control of a Turbulent Jet Using Periodic Excitation”, (previously AIAA paper 2002-3073), J. Propulsion and Power,
V19, N4, Jul-Aug 2003, pp. 646-654.
20.
Seifert,
A. and Pack, L.G., “Effects of Sweep on the Dynamics of Active Separation
Control”, Aeronautical J., 107 (1076): pp. 617-629, Oct 2003.
21.
Pack,
L.G. and Seifert, A., “Multiple Mode Actuation of a Turbulent Jet”, J.
Propulsion and Power, V20, N3, May-June 2004, pp. 572-575.
22.
Collis, S.S., Joslin, R.D, Seifert, A. and
Theofilis, V., “Issues in active flow control: theory, simulation and
experiment”, Prog. Aero Sci., V40, N4-5, May-July 2004 (previously AIAA
paper 2002-3277).
23.
Seifert,
A., Greenblatt, D. and Wygnanski, I.J., “Active Separation Control: Fundamental
Principles, Current Status and Future directions”, Aerospace Science and
Technology. 8, Aug. 2004, pp. 569-589.
24.
Sade, J.,
Cinamon, U, Ar, A. and Siefert, A, “Gas flow into and within the middle ear”,
OTOL NEUROTOL 25: (5) 649-652. (Note: my name was spelled wrong, as indicated
above).
25.
Halfon,
E, Nishri, B., Seifert, A. and Wygnanski, I.,
“Effects of Elevated Free-stream Turbulence on active control of a Separation
Bubble”, J. Fluids Eng., V. 126, pp. 1015-1024, Nov. 2004.
26.
Margalit,
S., Greenblatt, D., Seifert A. and Wygnanski , I.,
“Delta Wing Stall and Roll Control using Segmented Piezoelectric Fluidic
Actuators”, (previously AIAA paper 2002-3270), AIAA J. of Aircraft,
May-June 2004.
27.
Pack Melton,
L.G., Schaeffler, N., Yao,
C.S. and Seifert, A., “Active Control of Flow Separation from the Slat Shoulder
of a Supercritical Airfoil”, J. of AIRCRAFT, 42 (5): 1142-1149 SEP-OCT
2005 (previously AIAA Paper
2002-3156).
28.
Pack
Melton, L.G., Yao,
C.S. and Seifert, A., “Active Control of Flow Separation from the Flap of a
Supercritical Airfoil”, AIAA J., 44 (1): 34-41 JAN 2006 (previously AIAA Paper
2003-4005).
29.
Seifert,
A. and L. Pack Melton, “Identification and control of turbulent boundary layer
separation”, included in the book horoning “100 years of boundary layer
research” and L. Prandtl centennial lecture., Meier, GEA, Sreenivasan, KR
and Heinemann, HJ (Eds.), Springer,
2006, pp. 199-208.
30.
Yehoshua,
T. and Seifert, A. “Active boundary layer tripping using oscillatory vorticity
generator”, Aerospace Science and Technology, 10 (3): 175-180 APR 2006.
31.
Yehoshua,
T. and Seifert, A. “Boundary Condition Effects on the Evolution of a Train of
Vortex Pairs in Still Air”, Aeronautical J., 110 (1109): 397-417 JUL 2006.
32.
Nahum, A.
and Seifert, A., “On the application of confined twin-jet instability to
micro-mixing enhancement", Phys. Fluids, 18 (6): Art. No. 064107
JUN 2006.
33.
Nahum, A.
and Seifert, A., “A technique for backward particle tracking in a flow
field", Phys. Rev. E, 74 (1): Art. No. 016701 Part 2 JUL 2006.
34.
Timor, I., Ben-Hamou, E., Guy, Y. and Seifert, A., “Maneuvering
Aspects and 3D Effects of Active Airfoil Flow Control”, (previously AIAA paper
2004-2614), special Issue of Flow, Turbulence and
Combustion on "Air-jet actuators and their use for flow control",
(2007), 78: 429-443.
35.
Stalnov, O., Palei,
V., Fono, I., Cohen K. and Seifert, A.,
"Experimental Validation of Sensor Placement for Control of a 'D' Shaped
Cylinder Wake", (previously AIAA paper 2005-5260), Experiments in
Fluids, (2007) 42: 531-542.
36.
Naim, A., Greenblatt,
D., Seifert A. and Wygnanski, I., “Active
Control of a Circular Cylinder Flow at Transitional Reynolds Numbers"
(part of AIAA Paper 2002-3070), special Issue of Flow, Turbulence and
Combustion on "Air-jet actuators and their use for flow control",
(2007), 78: 383-407.
37.
Ben-Hamou, E., Arad, E. and Seifert,
A.., “Generic Transport Aft-Body Drag Reduction Using Active Flow Control“,
(previously AIAA paper 2004-2509), special Issue of Flow,
Turbulence and Combustion on "Air-jet actuators and their use for flow
control", (2007), 78: 365-382.
38.
Palei, V.
and Seifert, A., "Effects of Periodic Excitation on the Flow around a
D-Shaped Cylinder at Low Reynolds Numbers", special Issue of Flow, Turbulence
and Combustion on "Air-jet actuators and their use for flow
control", (2007), 78: 409-428.
IN PRESS
SUBMITTED
39.
Yehoshua,
T. and Seifert, A. “On the Evolution of Amplitude Modulated Train of Vortex
Pairs in Still Air”, Submitted to J. Fluid Mech., October 2005.
40.
Arwatz,
G., Fono, I. and Seifert, A., "Suction
and Oscillatory Blowing Actuator", submitted to AIAA J., Feb. 2007.
41.
Seifert,
A and Tilmann, C.P., "Fixed Wing Airfoil Applications", a chapter in
AIAA book series on "Active Flow Control", Eds. Joslin, RD and D.
Miller. April 2007.
42.
Stalnov,
O. and Seifert, A., "On amplitude scaling of active separation
control", submitted to Aeronautical J., July 2007.
43.
Levy,
D.E. and Seifert, A., “Simplified Dragonfly Airfoil Aerodynamics at Very Low
Reynolds Numbers”, submitted to the J. of Experimental Biology, November
2007.
IN PREPERATION
Five papers in
preperation (presented in AIAA and other meetings during 2005-7).
REVIEWED CONFERENCE PROCEEDINGS
1.
Seifert, A., “Non-linear
Evolution of Point-Source Disturbances in an Adverse Pressure Gradient Laminar
Boundary Layer”, Proceedings of IUTAM symposium on nonlinear instability and
transition in three-dimensional boundary layers, Manchester, UK,
1995. P.W. Duck and P. Hall (Eds.). pp. 187-196, Kluwer Academic Publishers,
1996.
2.
Seifert, A. and Tumin, A.,
“Non-linear Localized Disturbances in an Adverse Pressure Gradient Boundary
Layer Transition: Experiment and Linear Stability Theory”, Proceedings of the
8th Beer-Sheva symposium on Turbulence and MHD, 1996, published by AIAA
series Prog. In Aero. Sciences, 1999.
3.
Yehoshua, T. and Seifert, A.
“Active boundary layer tripping using oscillatory vorticity generator”, in
IUTAM Symposium on Laminar-Turbulent Transition : Proceedings of the Sixth
IUTAM Symposium on Laminar-Turbulent Transition, Bangalore, India, 2004,
Editor: Rama
Govindarajan.
4.
Seifert, A,
"Closed-loop AFC system: Actuators“. In KING, R.(Editor) : Active Flow
Control, Papers contributed to the Conference "Active Flow Control
2006", Berlin, Germany,
Springer-Verlag Berlin, NNFM (Notes on Numerical Fluid
Mechanics and Multidisciplinary Design) Volume 95, ISBN-10 3-540-71438-3, 2007.
5.
Seifert,
A. et al, “Large trucks drag reduction with active flow control”, paper
submitted to a book summerising the 2nd heavy vehicle drag reduction
conference, 2007. Eds. McCallen, Browand.
CONFERENCE PAPERS
1.
Shepshelovich, M., Koss, D.,
Wygnanski, I. and Seifert, A. “An Experimental Evaluation of Low Reynolds
number High-Lift Airfoil with Vanishingly Small Pitching Moment”, AIAA Paper
89-0538, 27th AIAA Aerospace Sciences Meeting, Jan. 1989.
2.
Seifert, A. and Wygnanski, I.,
“On the Interaction of Wave Trains Emanating from Two Point-Sources in a
Blasius Boundary Layer“, Proceedings of the boundary layer transition and
control conference, RAS, Cambridge, UK, April 1991.
3.
Seifert, A. Bachar, T.
Wygnanski, I., Koss, D. Shepshelovich, M.,
“Oscillatory Blowing, a Tool To Delay Boundary Layer Separation”, AIAA Paper
93-0440, 31st AIAA Aerospace Sciences Meeting, Jan. 1993.
4.
Koss, D., Bauminger, S.,
Shepshelovich, M., Seifert, A. and Wygnanski, I., “Pilot Test Of A Low Reynolds
Number DTE-airfoil”, AIAA Paper 93-0643, 31st AIAA Aerospace Sciences Meeting,
Jan. 1993.
5.
Seifert, A., Daraby, A., Nishri,
B. and Wygnanski, I., “The Effects of Forced
Oscillations on the Performance of Airfoils”, AIAA Paper 93-3264, AIAA Shear
Flow Conference, July 1993.
6.
Seifert, A., “Non-Linear,
Spanwise Interaction of Localized Disturbances in a Laminar Boundary Layer”,
paper included in the proceedings of “Minnowbrook I, Workshop on End-Stage
Boundary Layer Transition”, August 1993.
7.
Wygnanski, I.
and Seifert, A., “The Control Of Separation by Periodic Oscillations
(Invited)”, AIAA Paper 94-2608, 18th AIAA Aerospace Ground Testing Conference,
June 1994.
8.
Seifert, A., “Spot Calming
Effect on Boundary Layer Transition”, paper included in the proceedings of
“Minnowbrook II, Workshop on Boundary Layer Transition in Turbomachines”,
September 1997, NASA/CP-1998-206958, Eds. LaGraff, J.E. and Ashpis, D.E., pp.
99-110.
9.
Seifert, A. and Pack, L. G.,
“Oscillatory Control of Separation at High Reynolds Numbers (Invited)”, AIAA
Paper 98-0214, 36th AIAA Aerospace Sciences Meeting, Jan. 1998.
10.
Seifert, A. and Pack, L.G.,
“Oscillatory Excitation of Unsteady Compressible Flows over Airfoils at Flight
Reynolds Numbers”, AIAA paper 99-0925, 37th AIAA Aerospace Sciences Meeting,
Jan. 1999.
11.
Pack, L.G. and Seifert, A.,
“Periodic Excitation for Jet Vectoring and Enhanced Spreading”, AIAA paper
99-0672, 37th AIAA Aerospace Sciences Meeting, Jan. 1999.
12.
Rediniotis, O.K., Johansen,
E.S., Tsao, T, Seifert, A. and Pack, L. G., “MEMS-Based Probes for Velocity and
Pressure Measurements in Unsteady and Turbulent Flow Fields”, AIAA Paper
99-0521, 37th AIAA Aerospace Sciences Meeting, Jan. 1999.
13.
Seifert, A. and Pack, L.G.,
“Active Control of Separated Flows on Generic Configurations at High Reynolds
Numbers (Invited)”, AIAA paper 99-3403, presented at the AIAA 1999 Summer
Conferences, Norfolk, Va, Jun. 99. (1999 AIAA Best paper award by the
Fluid Dynamics TC).
14.
Seifert, A. and Pack, L.G.,
“Sweep & Compressibility Effects on Separation Control at High Re Numbers”,
AIAA paper 2000-0410, presented at the 38th AIAA Sciences Meeting, Reno, NV,
Jan. 2000.
15.
Pack, L.G. and Seifert, A.,
“Dynamics of Active Separation Control at High Re Number Turbulent Flows”, AIAA
paper 2000-0409, presented at the 38th AIAA Sciences Meeting, Reno, NV, Jan.
2000.
16.
Seifert, A. and Pack, L.G.,
“Separation Control at Flight Reynolds numbers: Lessons learned and Future
directions”, AIAA paper 2000-2542, presented at the AIAA Fluids 2000 Meeting,
Denver, CO, June 2000.
17.
Pack, L.G. and Seifert, A.,
“Multiple mode actuation of a turbulent Jet”, AIAA paper 01-0735, 39th AIAA
Aerospace Sciences Meeting, Jan. 2001.
18.
Seifert, A., Presented an
invited paper at the World Aviation Congress, Seattle, OR,
Sep. 2001.
19.
A. Naim, A. Seifert and I. Wygnanski,
“Active Control of Cylinder Flow With and Without a Splitter Plate Using
Piezoelectric Actuators”, AIAA Paper 2002-3070, June 2002.
20.
L. Pack, N.
Schaeffler, C. Yao and A. Seifert, “Active Control of Flow
Separation from the Slat Shoulder of a Supercritical Airfoil”, AIAA Paper
2002-3156, June 2002.
21.
Seifert, A., Joslin, R.D and
Theofilis, V., “Flow Control Experiments, Simulation and Modeling Approaches
(Invited)”, AIAA paper 2002-3277, presented at the AIAA 1st Flow Control
Meeting, , June 2002.
22.
D. Rapoport, I. Fono, K. Cohen
and Seifert, A., “Closed-loop Vectoring Control of a Turbulent Jet Using
Periodic Excitation”, AIAA paper 2002-3073, presented at the AIAA 1st Flow
Control Meeting, , June 2002.
23.
S. Margalit, D. Greenblatt, A.
Seifert and I. Wygnanski , “Active
Flow Control of a Delta Wing at High Incidence Using Segmented Piezoelectric
Actuators”, AIAA paper 2002-3270, presented at the AIAA 1st Flow Control
Meeting, , June 2002.
24.
L. Pack and C. Yao and A.
Seifert, “Active Control of Flow Separation from the Flap of a Supercritical
Airfoil”, AIAA paper 2003-4005, June 2003.
25.
Yehoshua, T. and Seifert, A.
“Boundary Condition Effects on Oscillatory Momentum Generator”, AIAA Paper
2003-3710, June 2003.
26.
L. Pack and C. Yao
and A. Seifert, “Application of Excitation from Multiple Locations on a
Simplified High-Lift System”, AIAA paper 2004-2324 , 2nd AIAA Flow Control
Conference, Portland, Oregon, June 28-1, 2004
27.
K. Cohen, ; S.
Siegel, M. Luchtenburg and T. McLaughlin and A. Seifert, “Sensor Placement for
Closed-Loop Flow Control of a "D" Shaped Cylinder Wake” AIAA paper 2004-2523,
2nd AIAA Flow Control Conference, Portland,
Oregon, June 28-1, 2004
28.
E. Ben-Hamou, E. Arad
and A. Seifert, “Generic Transport Aft-Body Drag Reduction Using Active Flow
Control“, AIAA paper 2004-2509 , 2nd AIAA Flow Control Conference, Portland,
Oregon, June 28-1, 2004
29.
I. Timor, E.
Ben-Hamou, Y. Guy, and A. Seifert, “Maneuvering Aspects and 3D Effects of
Active Airfoil Flow Control”, AIAA paper 2004-2614, 2nd AIAA Flow Control
Conference, Portland, Oregon, June 28-1, 2004
30.
A. Seifert and L.
Pack,”Identification and control of turbulent boundary layer separation”, Paper
presented at the IUTAM meeting honoring 100 years of boundary layer research
and Pradtl’s pioneering lecture, Goettingen, Germany, 12-14, Aug. 2004.
31.
Nahum A. and Seifert,
A., “Exploiting the confined twin-jet instability for micro mixing enhancement“,
IMECE paper 61648, Proceedings
of IMECE2004, 2004 ASME International Mechanical Engineering Congress and
RD&D Expo, November 13-19, 2004, Anaheim, California USA.
32.
Yehoshua, T. and
Seifert, A. “Active boundary layer tripping using oscillatory vorticity
generator”, Paper presented in the IUTAM symposium on laminar-turbulent
transition, Bangalore, India, December 2004).
33.
Yehoshua, T. and
Seifert, A. “On the evolution of amplitude modulated excitation in still air”,
Paper presented at the Israeli Aeronatics and Astronautics conferefce, Feb.
2005).
34.
Yom-Tov, Y. and
Seifert, A., Multiple Actuators Flow Control over a Glauert type Airfoil at Low
Reynolds Numbers, AIAA paper 2005-5389. June 2005.
35.
Stalnov, O., Palei, V.,
Fono, I., Cohen K. and Seifert, A., Experimental Validation of Sensor Placement
for Control of a "D" Shaped Cylinder Wake, AIAA paper 2005-5260, June
2005.
36.
Seifert, A. and
Arwatz, G., Actuators and Actuation approaches for effective flow control,
Paper presented at the Kat-Net meeting
on innovative technology in Aerodynamics,
Bremen, Germany,
June 20-22, 2005.
37.
Palei and Seifert, CFD paper ISR Aero Mtg, 3/06
38.
Yehoshua and Seifert,
PS cross flow paper, ISR Aero Mtg, 3/06
39.
Arad, Berkovitsy, Yehoshua and Seifert, ISR Aero Mtg, 3/06
40.
Arwatz, G., Fono, I. and Seifert, A., "Suction and Oscillatory Blowing
Actuator", London MEMS-IUTAM meeting, September 2006. (Proceedings to
appear).
41.
Yehoshua, T. and
Seifert, A. “On the receptivity of a boundary layer to high-amplitude
excitation (Invited)”, AIAA paper 2007-3994, June, 2007.
42.
Seifert, A. et al, Invited,
Heavy Vehicles Drag Reduction conference, Lake Taho,
CA., Aug. 2007.
43.
Seifert et al, Trucks
drag reduction, Reno
Jan 2008.
44.
Stalnov et al, ISR
Aerospace Conf., Feb 2008.
OTHER PUBLICATIONS
Presented and co-authored more than 68 papers (including
the above 45) at International scientific conferences wrote about 55 professional
research reports and presented about 42 seminars.
