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Old 5th Dec 2011, 14:29
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Vy vs Vx

hello folks

i am a bit puzzled, maybe at one point in my career i knew this but know i dont really remember it, i guess that is what reviews are for!!
anyway i know for a fact that Vy the best rate of climb speed decreases with altitude while Vx the best climb angle speed increases with altitude.
What is the reason behind that?

many thanks even though i am not positive this is the right section where to post my question!!

baobab
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Old 5th Dec 2011, 19:44
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Hi

Was subject of recent thread

Last edited by oggers; 5th Dec 2011 at 19:45. Reason: spelling
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Old 6th Dec 2011, 19:38
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Max angle/rate of climb speeds vary with altitude.True Air Seed(TAS) increases with altitude, that same Indicated Speed(IAS) you had at the sea level will not be enough to sustain given angle/rate of climb up at the high altitude. Wing senses only the TAS, however as pilots our primary reference is IAS.
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Old 6th Dec 2011, 20:15
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Hi all,

could vx and vy be same speed? It is that possible?
How do they change with altitude?

Thanks
Michelda
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Old 6th Dec 2011, 21:19
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could vx and vy be same speed?
Theoretically they should be @ same speed at the airplane's aboslute ceiling.
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Old 6th Dec 2011, 21:36
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At that altitude, "Quick" and "Fast" have the same meaning, eh?
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Old 8th Dec 2011, 00:07
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Hi vladko,

And what about at mean sea level?
Is it possibile?

Michelda
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Old 8th Dec 2011, 02:16
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Yes - if Sea Level happens to be the aircraft's absolute altitude. Although if that were the case you'd have greater worries such as trying to get airborne first.
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Old 8th Dec 2011, 05:07
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Take a look of p2006 flight manual and you get a surprise......
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Old 8th Dec 2011, 07:01
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michelda, I guess Tinstaafl answered the question for me Well that would be major engineering mishap!
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Old 8th Dec 2011, 20:07
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Vladko, don't the wings senses pressure (IAS) and not speed (TAS) or am I confussed here?

And don't you have to increase your TAS to maintain the same IAS not the other way around or...?
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Old 8th Dec 2011, 21:26
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Yes. Excuse me for phrasing it wrong. Wing senses pressure, and to maintain that same pressure at higher altitudes TAS has to be increased.
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