1.
Lachmann
,
G. V.
, 1961,
Boundary Layer and Flow Control. Its Principles and Application
,
Pergamon Press
,
New York
.
2.
Simpson
,
R. J.
, 1966, “
Aspects of Turbulent Boundary Layer Separation
,”
Prog. Aeronaut. Sci.
0079-6026,
32
, pp.
457
521
.
3.
Chang
,
P. K.
, 1976,
Control of Boundary Layer Separation
,
McGraw-Hill
,
New York
.
4.
Bragg
,
M. B.
, and
Gregorek
,
G. M.
, 1987, “
Experimental Study of Airfoil Performance with Vortex Generators
,”
J. Aircr.
0021-8669,
4
, pp.
305
309
.
5.
Simpson
,
R. Y.
, 1989, “
Turbulent Boundary Layer Separation
,”
Annu. Rev. Fluid Mech.
0066-4189,
21
, pp.
205
234
.
6.
Gad-el-Haq
,
M.
, and
Bushnell
,
D. M.
, 1991, “
Separation Control: Review
,”
J. Fluids Eng.
0098-2202,
113
, pp.
1
28
.
7.
Gad-el-Haq
,
M.
, 2000,
Flow Control
,
Cambridge University Press
,
Cambridge, UK
.
8.
Rao
,
D. M.
, and
Koriya
, 1988, “
Boundary-Layer Submerged Vortex Generators for Separation Control—An Exploratory Study
,” AIAA Paper 88-3546CP, pp.
839
846
.
9.
McCormick
,
D. C.
, 1993, “
Shock/Boundary-Layer Interaction Control with Vortex Generation and Passive Cavity
,”
AIAA J.
0001-1452,
31
(
1
), pp.
91
96
.
10.
Wallis
,
R. A.
, and
Stuard
,
C. M.
, 1962, “
On the Control of Shock-Induced Boundary Layer Separation with Discrete Air Jets
,” Aerodynamic Research Council C.P. No. 595.
11.
Johnson
,
J. P.
, and
Nishi
,
M.
, 1990, “
Vortex Generator Jets—Means for Flow Separation Control
,”
AIAA J.
0001-1452,
28
(
6
), pp.
989
994
.
12.
Szumowski
,
A.
, and
Wojciechowski
,
J.
, 2005, “
Use of Vortex Generators to Control Internal Supersonic Flow Separation
,”
AIAA J.
0001-1452,
43
(
1
), pp.
216
218
.
13.
Urzynicok
,
F.
, 2003, “
Separation Control by Flow-Induced Oscillations of a Resonator
,” Ph.D. thesis, T.U. Berlin, D83; edocs.tu-berlin.de/diss/2003/urzynicko_frank.htmedocs.tu-berlin.de/diss/2003/urzynicko_frank.htm
14.
Greenblatt
,
D.
, and
Wygnanski
,
I. J.
, 2000, “
The Control of Flow Separation by Periodic Oscillation
,”
Prog. Aerosp. Sci.
0376-0421,
36
, pp.
487
545
.
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