As a subsonic aircraft speeds-up, its Centre of Pressure
- moves aft.
- moves forward.
- is unaffected.
mahir asking:
explanation please?
Community Comments (2)
D
dimky Posts: 513 27.06.2014 / 10:01
Assuming that the aircraft is to remain at constant altitude, it must reduce its angle of attack as it speeds-up. This alone
will move the CofP rearwards, in accordance with the sub-sonic angle of attack change theory.
will move the CofP rearwards, in accordance with the sub-sonic angle of attack change theory.
M
mahir Posts: 1 27.06.2014 / 13:49
Thanks for your feedback dimky,
appreciated!!
appreciated!!
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