Environmental Engineering Reference
In-Depth Information
modification with reinforcement of
the profile structure and development
and installation of electronic sensors
1 000 t less fuel consumption
per year, which is approximately 25 %
fuel reduction
integrated winglet
reduced noise
modification in approximately 25 days
variable profile curvature
more effective lifting system
by low velocity
Fig. 7.4
Wing of a middle distance airplane with raked wingtips
airplanes. The reduced aerodynamic resistance always leads to decreased fuel
consumption and exhaust gas emissions [ 11 ]. Development of a porous surface of
airplanes is a high risk technical challenge. Contamination by insects and debris
can significantly reduce the performance of laminar flow and increase maintenance
costs. Therefore more time is needed before it can be introduced [ 12 ].
7.3 Hydro- and Aerodynamics of Ships
The ship's fuel consumption depends on the function:
FC ¼ c R q w
2
v 2 S :
ð 7 : 1 Þ
In the function c R is the resistance coefficient, q w the density of water, v the
speed of the ship and S the moistened surface. The resistance coefficient c R can be
relatively easily tested and exactly determined for cars and airplanes, but not for
ships because ships move through both the water and the air. The resistance is the
sum of both determining factors [ 13 ].
There
are
different
basic
types
of
approach
to
assess
the
hydrodynamic
resistance:
• Testing in a basin;
• Testing in wind tunnels; and
• Using a computer model [ 14 ].
Search WWH ::




Custom Search