Abstract: Team pursuit is a relatively new event in international
long track speed skating. For a single speed skater the aerodynamic
drag will account for up to 80% of the braking force, thus reducing
the drag can greatly improve the performance. In a team pursuit the
interactions between athletes in near proximity will also be essential,
but is not well studied. In this study, systematic measurements
of the aerodynamic drag, body posture and relative positioning
of speed skaters have been performed in the low speed wind
tunnel at the Norwegian University of Science and Technology, in
order to investigate the aerodynamic interaction between two speed
skaters. Drag measurements of static speed skaters drafting, leading,
side-by-side, and dynamic drag measurements in a synchronized and
unsynchronized movement at different distances, were performed.
The projected frontal area was measured for all postures and
movements and a blockage correction was performed, as the blockage
ratio ranged from 5-15% in the different setups. The static drag
measurements where performed on two test subjects in two different
postures, a low posture and a high posture, and two different distances
between the test subjects 1.5T and 3T where T being the length of the
torso (T=0.63m). A drag reduction was observed for all distances and
configurations, from 39% to 11.4%, for the drafting test subject. The
drag of the leading test subject was only influenced at -1.5T, with
the biggest drag reduction of 5.6%. An increase in drag was seen
for all side-by-side measurements, the biggest increase was observed
to be 25.7%, at the closest distance between the test subjects, and
the lowest at 2.7% with ∼ 0.7 m between the test subjects. A clear
aerodynamic interaction between the test subjects and their postures
was observed for most measurements during static measurements,
with results corresponding well to recent studies. For the dynamic
measurements, the leading test subject had a drag reduction of 3%
even at -3T. The drafting showed a drag reduction of 15% when being
in a synchronized (sync) motion with the leading test subject at 4.5T.
The maximal drag reduction for both the leading and the drafting
test subject were observed when being as close as possible in sync,
with a drag reduction of 8.5% and 25.7% respectively. This study
emphasize the importance of keeping a synchronized movement by
showing that the maximal gain for the leading and drafting dropped to
3.2% and 3.3% respectively when the skaters are in opposite phase.
Individual differences in technique also appear to influence the drag
of the other test subject.
Abstract: A new mechanism responsible for structural life
consumption due to resonant fatigue in turbine blades, or vanes, is
presented and explained. A rotating blade or vane in a gas turbine can
change its contour due to erosion and/or material build up, in any of
these instances, the surface pressure distribution occurring on the
suction and pressure sides of blades-vanes can suffer substantial
modification of their pressure and temperatures envelopes and flow
characteristics. Meanwhile, the relative rotation between the blade
and duct vane while the pressurized gas flows and the consequent
wake crossings, will induce a fluctuating thrust force or lift that will
excite the blade.
An actual totally used up set of vane-blade components in a HP
turbine power stage in a gas turbine is analyzed. The blade suffered
some material erosion mostly at the trailing edge provoking a
peculiar surface pressure envelope which evolved as the relative
position between the vane and the blade passed in front of each other.
Interestingly preliminary modal analysis for this eroded blade
indicates several natural frequencies within the aeromechanic power
spectrum, moreover, the highest frequency component is 94% of one
natural frequency indicating near resonant condition.
Independently of other simultaneously occurring fatigue cycles
(such as thermal, centrifugal stresses).