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Old 26th January 2021 | 07:32
  #21 (permalink)  
 
Joined: Apr 2010
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From: IRS NAV ONLY
Originally Posted by pineteam
And why on heavy weight the V1,Vr V2 speeds are higher on conf 3 versus conf 2 but not on light aircraft?
thank you.
When heavy and with more drag, you are likely to be performance-limited at 2nd segment. V2min is normally way below Vx, so increasing VR/V2 where runway length permits will improve 2nd segment performance.

With light aircraft, you are unlikely to be limited, so V2 will be V2min, which is obviously lower for a configuration with more lift at low speeds (CONF 3).
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Old 26th January 2021 | 08:44
  #22 (permalink)  

Only half a speed-brake
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From: Commuting not home
IIRC the calculation searches for results with the best gradient (the highest permissible tkof weight in disguise). So to overcome the drag penalty of F3, higher V2 is chosen - it suggests that it climbs better with higher speed.

Aero theory supports that. Max L/D for a given configuration is pretty constant but in order to achieve it higher speeds are needed for higher weights. Perhaps F2 does not drag that much and the markedly higher speeds are not needed. Yet second-guessing an iterative algorithm is rather pointless.
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Old 27th January 2021 | 07:01
  #23 (permalink)  
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You guys rock! Thank you!
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