At 05:52 PM 31/01/2007, you wrote:
Good work Ken.. Reminds me of the time you worked out that a Ka6
could not fly above 96,000 feet because the Vne equaled the stalling
speed.. good memories from 40 years ago. :)
I suspect the limiting mach number would make it somewhat les than 96000 feet.
If you want to be really fussy about the water column you should
correct the density of the water for temperature.
Mike
Borgelt Instruments - manufacturers of quality soaring instruments
phone Int'l + 61 746 355784
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cellphone Int'l + 61 428 355784
Int'l + 61 429 355784
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