WARNING! READING MIGHT CAUSE A HEADACHE.
So far I've been to lazy to do another experiment, so I've been thinking about it a bit.
the theory is this:
consider the plane as a chunk of mass "m" moving straight up with a pulling force "F" (prop) against garvity "mg" and drag "d".
we'll assume body drag only, neglecting aerodynamic effects (wing tip turbulance, etc.) due to low attack angle in the vertical.
so " d=jx' " where:
x' = velocity (first time derivative of distance)
j = drag constant.
it's an over simplification but i think that's enough to get the idea.
if a=x" is acceleration, we get:
ma=mx"=F-mg-jx'
which is a diff. equation of the form: x" + Ax' = B
well, you got the idea. so to save time and key strokes, the solution is:
x=[(F-mg)/j - V](m/j)*exp{-t*(j/m)} + t*(F-mg)/j + H
V = initial speed.
H = constant calibration for initial alt.
if we plot this function we get a sum of an exponent and a line with a single maxima.
results:
1. m/j - we see (as one might expect) that the ratio m/j appears several times. so as for body mass and drag what matters is the ratio.
the higher the better. a drag efficient but relatively light AC would not benefit much of that factor.
BUT, the higher you are, j gets smaller! so high m/j planes should enjoy this.
2. F-mg (negetive value) - how big an engine comparing with weight.
this is a dominant factor, and gets more important as j increases (at low alt).
light strong planes should benefit here (yak as an example?).
this enables them to stay longer almost stopped at the top.
maybe this explanes the yak preformance at the experiment.
3. V - initial speed.
effects the exponent term only (ruled by m/j ratio). so this also work for better m/j planes.
conclusion:
1. high m/j AC makes a good vertical fighter and gets better with alt and speed.
for some conditions, being loaded with internal fuel might actually help here.
2. Big engine + small plane? advantage at low alt and not too high speeds. (not to mention smoother manuver).
3. the experiment was in bad conditions for the jug. but i still think the result is poor.
4. more testing is needed to verify the above (and of course - we don't have the exact data to apply here).
i'll test that and report.
Bozon
332 Vikings Squad