Quoting naruto38700 (Thread starter):
The problem is, I know that those factors are there, but still no idea how they influence runway length numerical. Is there a formula to quantify the most optimum runway length using those stats? |
There is no formula. What you need are the lookup tables for takeoff performance.
Quoting naruto38700 (Thread starter): For instance, lets say we have prevailing wind 050° at 20 knots, critical aircraft is A380 with the stage length of 13,500 km. What runway length will it be then? |
About 9200'.
13500 km is into the part of the payload/range curve on an A380-800 where you have to take a payload restriction to carry enough fuel, so we assume you're at MTOW. MTOW on the A380-800 varies wildly depending on which specific aircraft you're talking about, but we assume 575,000 kg as the high end. At that weight, 0', ISA standard day, you need 9200' minimum (full thrust takeoff, using the whole runway). More would be better. You don't take credit for wind for runway planning because you can't count on it. If the runway is at altitude or it's a hot day, you need more length.
All the information you need for a question like this (to get a rough answer) can be found in the ACAP documents:
http://www.airbus.com/fileadmin/medi...ata/AC/Airbus-AC_A380_20121101.pdf
Tom.