Laminarflow
Re
MPkinematicviscosity
I Yiff turn
Re Recrit laminar
Re Recrit turbulent
Recrit
tin
Pipe 2200
1500000
sphere
Recrit
Boundary Layers
fundamentalflowtype onlyforviscousflow
Boundarylayers
shearlayers
wakes
Boundarylayerthickness no
8 0.9900
on flatplategrows withdistance
, DisplacementThickness
Ua
Area Vo a
ay
Δ
8
8 1 g dy displacementthickness
MomentumThickness
0 1 1
8 dy
Blasius Boundary Layers Thickness
Laminar Flat plate
Special case
mindhow
spy
81 5
ftp.ptessure
gradient
e
no
Rex
i iii
ysneaiiiisiii.ie
srintriti.n
o.am of o.oo
u i Un
i jii
ient
Cf
0.664
Rex
or
f
Ct 0002
ooo
fnn.to
I t.ae 2.0106 soto woke
Rex