Extending range: options and opinion
Posted: 06 Oct 2007, 00:04
HI all,
I'd like to put forward some of my theories and experiences for extending range in flights on FS (and possibly in real life?) - and how they compare to the 'real thing'.
Here goes:
I'm aware that generally, we want to be going as high and as (reasonably) fast as we can to get mximum efficiency.
My question was/is - how to go about this?
For the purposes of this exercise of course we must assume total airspace clearance with permission to climb/descend and route at will.
I have tested differing climb techniques, but, I find that for a given fuel load, it is very, very hard to compar like with like. For example, a plane loaded with 20% fuel will reach FL350 much more easily than an A/C with more fuel - so trying to vary the climb technique does not work on light loads.
In ideal conditions, it would appear (to me) that an aircraft correctly flown *should* gain maximum range with slightly *less* than maximum TOW. (We will call TOW fuel load only for this exercise).
The above is on the theory that with less weight to lift, to a given height, once at optimum altitude the plane will have roughly the same load, given it has had less effort to get there.
But, assuming a total load, what do we do to extend?
Despite advice and theory saying 'get to FLXXX' quickly, I have found with numerous flights that I can achive hugely greater ranges with the 'slow climb' technique. I will perform a standard takeoff, and once above FL100 trim the aircraft into a 1500fpm climb. Taking the Super 10, I then take this down 50% at FL200, and another 50% at FL250. Once FL300 is reached I level off, and wait until the fuel is down to 70% load. Then I initiate a climb at 100fpm, and leave this until FL 425 is reached when I level off. I have found no other way to extend range further. I find that while the plane may be a little heavy to sneak above FL300 at that weight, it is countered by the fact that 100fpm is such a slight climb that it does not affect speed, and gives optimum endurance.
The descent is calculated at 800fpm with distance to go vs altitude, to FL100 when I self-impose the 250kt restriction and then adjust descent to needs.
This allows a 'clean' descent with reasonable speed.
Does any of this make any sense? :roll:
I'd like to put forward some of my theories and experiences for extending range in flights on FS (and possibly in real life?) - and how they compare to the 'real thing'.
Here goes:
I'm aware that generally, we want to be going as high and as (reasonably) fast as we can to get mximum efficiency.
My question was/is - how to go about this?
For the purposes of this exercise of course we must assume total airspace clearance with permission to climb/descend and route at will.
I have tested differing climb techniques, but, I find that for a given fuel load, it is very, very hard to compar like with like. For example, a plane loaded with 20% fuel will reach FL350 much more easily than an A/C with more fuel - so trying to vary the climb technique does not work on light loads.
In ideal conditions, it would appear (to me) that an aircraft correctly flown *should* gain maximum range with slightly *less* than maximum TOW. (We will call TOW fuel load only for this exercise).
The above is on the theory that with less weight to lift, to a given height, once at optimum altitude the plane will have roughly the same load, given it has had less effort to get there.
But, assuming a total load, what do we do to extend?
Despite advice and theory saying 'get to FLXXX' quickly, I have found with numerous flights that I can achive hugely greater ranges with the 'slow climb' technique. I will perform a standard takeoff, and once above FL100 trim the aircraft into a 1500fpm climb. Taking the Super 10, I then take this down 50% at FL200, and another 50% at FL250. Once FL300 is reached I level off, and wait until the fuel is down to 70% load. Then I initiate a climb at 100fpm, and leave this until FL 425 is reached when I level off. I have found no other way to extend range further. I find that while the plane may be a little heavy to sneak above FL300 at that weight, it is countered by the fact that 100fpm is such a slight climb that it does not affect speed, and gives optimum endurance.
The descent is calculated at 800fpm with distance to go vs altitude, to FL100 when I self-impose the 250kt restriction and then adjust descent to needs.
This allows a 'clean' descent with reasonable speed.
Does any of this make any sense? :roll: