South west Scotland has been a no-fly zone for the last five weeks or so because folks in the Caribbean keep sending us their used hurricanes - their latest offering was called Abigail, but there are others queued up behind her like city buses to somewhere you don't want to go.
So, "cabin fever" is taking hold here and I've been wondering (thinking is too grand a word) about back-country landing site evaluation, especially for steeply-sloping strips.
The first question is obviously "can I take off from there?", but I'm going to dodge that issue for the time being.
The next question is "can I land there in one piece?", which boils down to two considerations:
- Is the landing surface suitable?
- Is the landing site long enough for my airplane in the current conditions?
We can inspect the surface and in some cases feel or "drag" it, which is usually satisfactory - although some granular materials can surprise after we're stopped (how to detect quicksand, for instance?).
The traditional (FAA/CAA) way to estimate ground roll required is to look in the Airplane Flight Manual for data complied on a flat lowland concrete runway by some long-dead test pilot and extrapolate from that by piling on a heap of approximate "fudge factors" for aircraft mass, density altitude, tail-wind, runway slope, runway surface (grass, gravel, wet or dry), and... have I forgotten something, apart from the fact that I would search in vain for any kind of performance data in my AFM...
Armed with this fine approximation of an approximation of the approximate landing roll required by an approximately similar airplane we can do what? I think most of us just look at a back-country landing site and use our experience to judge "GO" or "NO-GO".
That kind of gut-feeling served the world's engineers pretty well until Galileo and Newton came along to analyse how a pendulum works and why an apple drops from a tree, but now that we learn that good stuff in school, why not put it to use for flying in the back-country?
Jacko's thesis, somewhat inspired by the aforementioned cabin fever, is that we can make a decent stab at landing site evaluation by carrying out a simple in-flight stall test and then applying the principle of conservation of energy:
Kinetic energy at touch-down (KE) = potential energy gained running up the slope (PE) + work done against the brakes (Work)
(Note that if KE is less than PE, then instead of braking we will use some engine power to get up the slope).
KE = 1/2 m V^2 (0.5 times MASS times TOUCH-DOWN SPEED squared)
PE = m g H (MASS times ACCELERATION DUE TO GRAVITY times HEIGHT GAINED)
Work = F D (BRAKING FORCE times GROUND ROLL DISTANCE)
But maximum braking force is = m g µ, where µ is the coefficient of friction between tire and runway surface
So we can write our energy equation as:
1/2 m V^2 = (m g H) – (m g Cf D)
Dividing by m and re-arranging we have:
µ = (((V^2)/(2 g))-H)/D
We can estimate touch-down speed V directly from GPS ground speed with the airplane stalled at a safe height above the runway. This allows for density altitude, but we may need to allow a little more or less for wind speed at ground level, and of course stall in ground effect is a few knots slower than in free air.
The formula tells us (in theory) whether we can stop in the available runway length with the main wheel braking friction estimated to be available/usable according to the "runway" surface and aircraft configuration.
In case anyone has got this far, I've put a spreadsheet calculation of the above formula at:
https://docs.google.com/spreadsheets/d/ ... cslist_api
...and I'd be interested to know if anyone else finds it (a) reasonably accurate or (b) any better than just eyeballing and voting yes or no.
I'm afraid this is in metric units, but I can easily do a version in US units (feet instead of meters).




