Boundary-layer separation can be prevented or delayed by sucking part of the boundary layer into the surface, but in a straightforward application the required hydraulics entail significant penalties in terms of weight and cost. By means of computational techniques, this paper explores the possibility of autogenous suction, in which the local pressure differences that lead to separation drive the suction used to prevent it. The chosen examples include steady and unsteady laminar flows around leading edges of thin airfoils. No fundamental theoretical limit to autogenous suction was found in the range of angles of attack that could be studied, but rapidly increasing suction volumes suggest that practical application will become increasingly difficult for more severe adverse pressure gradients.

1.
McAlister
,
K. W.
, and
Carr
,
L. W.
, 1979, “
Water Tunnel Visualizations of Dynamic Stall
,”
ASME J. Fluids Eng.
0098-2202,
101
, pp.
367
380
.
2.
Francis
,
M. S.
, and
Keesee
,
J. E.
, 1985, “
Airfoil Dynamic Stall Performance With Large Amplitude Motions
,”
AIAA J.
0001-1452,
23
, pp.
1653
1659
.
3.
Acharya
,
M.
, and
Metwally
,
M. H.
, 1992, “
Unsteady Pressure Field and Vorticity Production Over a Pitching Airfoil
,”
AIAA J.
0001-1452,
30
, pp.
403
411
.
4.
Currier
,
J. M.
, and
Fung
,
K.-Y.
, 1992, “
Analysis of the Onset of Dynamic Stall
,”
AIAA J.
0001-1452,
30
, pp.
2469
2477
.
5.
Shih
,
C.
,
Lourenco
,
L. M.
,
Van Dommelen
,
L. L.
, and
Krothapalli
,
A.
, 1992, “
Unsteady Flow Past an Airfoil Pitching at Constant Rate
,”
AIAA J.
0001-1452,
30
, pp.
1153
1161
.
6.
Karim
,
M. A.
, and
Acharya
,
M.
, 1994, “
Suppression of Dynamic Stall Vortices Over Pitching Airfoils by Leading-Edge Suction
,”
AIAA J.
0001-1452,
32
, pp.
1647
1655
.
7.
Wang
,
S.-C.
, 1995, “
Control of Dynamic Stall
,” Ph.D. thesis, Florida State University, Tallahassee, FL.
8.
Yu
,
Y. H.
,
Lee
,
S.
,
McAlister
,
K. W.
,
Tung
,
C.
, and
Wang
,
C. M.
, 1995, “
Dynamic Stall Control for Advanced Rotorcraft Application
,”
AIAA J.
0001-1452,
33
, pp.
289
295
.
9.
Alrefai
,
M.
, and
Acharya
,
M.
, 1996, “
Controlled Leading-Edge Suction for Management of Unsteady Separation Pitching Airfoils
,”
AIAA J.
0001-1452,
34
, pp.
2327
2336
.
10.
Atik
,
H.
,
Kim
,
C.-Y.
,
Van Dommelen
,
L.
, and
Walker
,
J.
, 2005, “
Boundary-Layer Separation Control on a Thin Airfoil Using Local Suction
,”
J. Fluid Mech.
0022-1120,
535
, pp.
415
443
.
11.
Prandtl
,
L.
, 1961, “
Über Flüssigkeitsbewegung bei sehr kleiner Reibung
,”
Ludwig Prandtl gesammelte Abhandlüngen
,
Springer-Verlag
,
Berlin
, Vol.
2
, pp.
575
584
.
12.
Poppleton
,
E. D.
, 1955, “
Boundary Layer Control for High Lift by Suction of the Leading-Edge of a 40Degree Swept-Back Wing
,” ARC, UK, Technical Report No. RM 2897.
13.
1961,
Boundary Layer and Flow Control
,
G.
Lachmann
, ed.,
Pergamon
,
London
, Vols.
I
and
II
.
14.
Bahi
,
L.
,
Ross
,
J.
, and
Nagamatsu
,
H.
, 1983, “
Passive Shock Wave/Boundary Layer Control for Transonic Airfoil Drag Reduction
,” AIAA Paper No. 83-0137.
15.
Nagamatsu
,
H.
,
Dyer
,
R.
, and
Ficarra
,
R.
, 1985, “
Supercritical Airfoil Drag Reduction by Passive Shock Wave/Boundary Layer Control in the Mach Number Range .75 to .9
,” AIAA Paper No. 85-0207.
16.
Nagamatsu
,
H.
,
Trilling
,
T.
, and
Bossard
,
J.
, 1987, “
Passive Drag Reduction on a Complete NACA 0012 Airfoil at Transonic Mach Numbers
,” AIAA Paper No. 87-1263.
17.
Koval’nogov
,
S.
,
Fomin
,
V.
, and
Shapovalov
,
G.
, 1987, “
Experimental Study of the Possibility of Passive Control of Shock-Boundary Layer Interactions
,”
Uch. Zap. TsAGI
0321-3439,
18
, pp.
112
116
.
18.
Van Dyke
,
M.
, 1964,
Perturbation Methods in Fluid Mechanics
,
Academic
,
New York
.
19.
Zalutsky
,
K.
, 2000, “
Unsteady Boundary-Layer Separation
,” Ph.D. thesis, Lehigh University, Lehigh, PA.
20.
Werle
,
M. J.
, and
Davis
,
R. T.
, 1972, “
Incompressible Laminar Boundary Layers on a Parabola at Angle of Attack: A Study of the Separation Point
,”
ASME J. Appl. Mech.
0021-8936,
39
, pp.
7
12
.
21.
Terrill
,
R. M.
, 1960, “
Laminar Boundary Layer Flow Near Separation With and Without Suction
,”
Philos. Trans. R. Soc. London, Ser. A
0962-8428,
253
, pp.
55
100
.
22.
Van Dommelen
,
L. L.
, and
Shen
,
S. F.
, 1980, “
The Spontaneous Generation of a Singularity in a Separating Boundary Layer
,”
J. Comput. Phys.
0021-9991,
38
, pp.
125
140
.
23.
Van Dommelen
,
L. L.
, and
Cowley
,
S. J.
, 1990, “
On the Lagrangian Description of Unsteady Boundary-Layer Separation. Part 1. General Theory
,”
J. Fluid Mech.
0022-1120,
210
, pp.
593
626
.
24.
Panton
,
R.
, 2005,
Incompressible Flow
, 3rd ed.,
Wiley
,
Hoboken, NJ
.
25.
Doligalski
,
T. L.
, and
Walker
,
J. D. A.
, 1984, “
The Boundary Layer Induced by a Convected Vortex
,”
J. Fluid Mech.
0022-1120,
139
, pp.
1
28
.
26.
Peridier
,
V. J.
,
Smith
,
F. T.
, and
Walker
,
J. D. A.
, 1991, “
Vortex-Induced Boundary-Layer Separation. Part 1. The Unsteady Limit Problem Re→∞
,”
J. Fluid Mech.
0022-1120,
232
, pp.
99
131
.
27.
Degani
,
A. T.
,
Li
,
Q.
, and
Walker
,
J. D. A.
, 1996, “
Unsteady Separation From the Leading Edge of a Thin Airfoil
,”
Phys. Fluids
1070-6631,
8
, pp.
704
714
.
28.
Atik
,
H.
, 2002, “
Boundary-Layer Separation and Control
,” Ph.D. thesis, Lehigh University, Lehigh, PA.
29.
Lighthill
,
M. J.
, 1963, “
Introduction. Boundary Layer Theory
,”
Laminar Boundary Layers
,
L.
Rosenhead
, ed.,
Oxford University Press
,
Oxford, UK
, pp.
46
72
.
You do not currently have access to this content.