Closed GoogleCodeExporter closed 8 years ago
Original comment by daniel.b...@googlemail.com
on 9 Oct 2012 at 7:01
[deleted comment]
[deleted comment]
New version of altitude-to-Reynolds converted map (previous one involved some
extrapolation). In annotation the data point's altitude in km; chord length is
4.19 m.
Original comment by brsverv...@gmail.com
on 15 Oct 2012 at 2:16
Attachments:
We now do have several arguments for the discussion of altitude vs.
reynoldsnumber as the second parameter for the performance map in combination
with the mach number:
With the altitude the range of the values is certainly smaller. The
reynoldsnumbers need to be scaled from approx 2mio to 80mio to cover a complete
jet aircraft flight regime.
With the reynoldsnumber it might be a lot easier to work in different
atmospheres (ISA+15, ISA+30). This might become important as soon as we start
working on detailed starting and landing simulations. If these temerature
variations need to be included from the altitude, there might be a lot of
conversions.
Still no decision, but at least we might feel smarter
Original comment by daniel.b...@googlemail.com
on 24 Oct 2012 at 7:43
For CPACS 2.01 the aeroPerformancMap will stick to the Reynoldsnumber. For
takeoff filed length calculations at different ambient settings this seems to
be reasonable.
Original comment by daniel.b...@googlemail.com
on 30 Oct 2012 at 2:18
Original comment by daniel.b...@googlemail.com
on 27 May 2013 at 8:02
Original issue reported on code.google.com by
daniel.b...@googlemail.com
on 31 Aug 2012 at 7:27