On Tue, 19 Dec 2006, Maik Justus wrote:
Important info for the ch47d flight model. I had expected a large delta3
effect. Can you point me to the point in the report, where you found
this info?
From the British ministry of defence:
http://www.mod.uk/NR/rdonlyres/DB72A687-551F-498C-A402-A015E9C1CDDB/0/chinook_boeing1c.pdf
(~2.5MB A report regarding the simulation of the accident. They mention
several times that although the software used for the simulation is capable
of taking delta3 into account, this is not used for the reason that there
is no delta3 on the chinook helicopter.)
Another little gem in the same collection (haven't seen this one before
myself):
http://www.mod.uk/NR/rdonlyres/8BF9CD63-D369-47AD-88A1-0117FEE32C01/0/chinook_boeing1b.pdf
(a few diagrams of output from the simulation which gives away some data about
the
LCT algorithm -- it was 4°+4° after all. And Rotor thrust/torque in real
units.) Now I'm confused about the LCT again. 4° relative what? "their
respective masts"?? :P
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