We analyse the low-Reynolds-number flow generated by a cylinder (of radius
$a$
) in a stream (of velocity
$U_{\infty }$
) which has a uniform through-surface blowing component (of velocity
$U_{b}$
). The flow is characterized in terms of the Reynolds number
$Re$
(
$=2aU_{\infty }/{\it\nu}$
, where
${\it\nu}$
is the kinematic viscosity of the fluid) and the dimensionless blow velocity
${\it\Lambda}$
(
$=U_{b}/U_{\infty }$
). We seek the leading-order symmetric solution of the vorticity field which satisfies the near- and far-field boundary conditions. The drag coefficient is then determined from the vorticity field. For the no-blow case Lamb’s (Phil. Mag., vol. 21, 1911, pp. 112–121) expression is retrieved for
$Re\rightarrow 0$
. For the strong-sucking case, the asymptotic limit,
$C_{D}\approx -2{\rm\pi}{\it\Lambda}$
, is confirmed. The blowing solution is valid for
${\it\Lambda}<4/Re$
, after which the flow is unsymmetrical about
${\it\theta}={\rm\pi}/2$
. The analytical results are compared with full numerical solutions for the drag coefficient
$C_{D}$
and the fraction of drag due to viscous stresses. The predictions show good agreement for
$Re=0.1$
and
${\it\Lambda}=-5,0,5$
.
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