Download 00410233.pdf

Survey
yes no Was this document useful for you?
   Thank you for your participation!

* Your assessment is very important for improving the workof artificial intelligence, which forms the content of this project

Document related concepts

Flow measurement wikipedia , lookup

Cyclorotor wikipedia , lookup

Flow conditioning wikipedia , lookup

Wind power forecasting wikipedia , lookup

Computational fluid dynamics wikipedia , lookup

Bernoulli's principle wikipedia , lookup

Compressible flow wikipedia , lookup

Anemometer wikipedia , lookup

Wind-turbine aerodynamics wikipedia , lookup

Rheology wikipedia , lookup

Turbulence wikipedia , lookup

Fluid dynamics wikipedia , lookup

Aerodynamics wikipedia , lookup

Wind tunnel wikipedia , lookup

Reynolds number wikipedia , lookup

Transcript
The use of Aeronautical Experimental Facilities
and Measurement Techniques for the
Aerodynamic Investigation of High Speed
Trains
Andreas Dillmann
German Aerospace Center (DLR), Germany
[email protected]
Abstract The development of future high speed trains is driven by commercial
and ecological requirements which determine the increase of speed and payload
while reducing weight and improving thermal and acoustical passenger comfort.
To ensure the same level of safeness then for today’s rolling stock, additional issues like Reynolds-Number and Mach-Number dependencies have to be explored.
The influence of unsteady flow phenomena as well as the impact of the train’s induced flow field on humans and infrastructure has to be investigated. For this
purpose, special experimental facilities and techniques originally developed for
aeronautical research proved to be extremely useful. For the investigation of viscous flow effects like separation and other boundary layer phenomena, a pressurized wind tunnel can realize high Reynolds numbers without entering the compressible flow regime. Validated results for the Göttingen high pressure wind
tunnel show that it is possible to use extremely small models, down to a scale of
1:100, and to get good results if the accuracy of the model manufacturing process
is high enough. A second possibility to increase the Reynolds number in a wind
tunnel is to cool down the working fluid, thus increasing the Reynolds number up
to a factor of 5.5. The main advantage of cryogenic wind tunnels is the possibility
of independent adjustment of the Mach and Reynolds number. A third possibility
to increase the Reynolds number is to change the working fluid of the facility, e.g.
by using water instead of air. Advanced measurement techniques, which were
originally developed for aeronautical research, allow a deep insight into the physical mechanisms governing the aerodynamic performance of high speed trains. A
broad variety of experimental results is presented, showing that high Reynolds
number facilities are in many cases an indispensable research tool for the aerodynamics of railroad vehicles.