Idea Transcript
https://ntrs.nasa.gov/search.jsp?R=19980003835 2019-01-10T03:36:47+00:00Z
/IJ " > r,
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To expand stages
HIGH
on the results
of transition,
section
7:
presented
a case with a longer
was left in the geometry
the inlet velocity free-stream
was reduced
velocities
dUcw/dx=29
is changed.
numbers
and higher
to half the value
acceleration
As in the two high-FSTI
the present
case was two-dimensional below
are also available
EXPERIMENTAL
The free-stream
at ten streamwise
gradient
measurement
parameters,
Rex=8.Tx
105.
are listed
The acceleration
of the test wall to 0.80x10
airfoils
in Volino
and Simon
in Chapter
to half the values remains
doubled. to extend
described
in a time-averaged
the test section
velocity
important
modem
of the
constant
The lower
Some
(1994b,
as the
Reynolds zone
the boundary
sense.
6, and
the local
the transition
above,
in
layer
in
of the results
1995b,
1995c).
are roughly
of 5.2 rn/s and a nominal
was held at 14.35 s-1.
stations.
The locations
in Table
7.1.
parameter
Profile
of these
from K=8.6x station.
Reynolds
the same.
253
numbers
of
acquired with other
station,
10 -6 at the leading from
in Fig. 7.1.
the same as that of the CF6 airfoil,
The chord
along
The K profile
of Fig. 5.1 are shown
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_--_ E_ ;t,_ •.-..-,.: v,-, _ " ,_.:C
*
=
*.
v