denverpilot
Tied Down
I think people forget the u-shape...
Math is hard.
I think people forget the u-shape...
It's not really the same as an SP. Just the 180 HP engine is. Which doesn't matter if it's failed. For some reason, the ASI calibration is different for SPs at low speed (they read slower than older 172s, at the same CAS), so P's don't compare in IAS.
Max weight is also different, despite the same size engine and same flaps. P's are 2400 lb. SP's are 2550. N's are 2300 lb (but have 40 deg flaps).
With two up front and nothing else with full fuel, I'd be around 2000 lb in an N or P. Of course that will vary for the OP and for installed equipment. But that means a 20% reduction in gross weight, so V speed reduction is around 10%. That makes 63 KIAS fast.
Ok...at what point did I say trim flies the aircraft?I didn't say that you said that. Read it again carefully please.
Ok...at what point did I say trim flies the aircraft?
roughly 80% max weight, so adjusted best glide would be roughly 90% of the published number.
They are slightly different.wouldn't you expect a difference between N and P models then, too?
IAS doesn't measure AOA. Apparently the increased position error doesn't offset the increase in speed.It affects the stall speeds as well (in IAS), which are always at the same angle of attack when clean (as these models have the same wing).
Math is hard.
roughly 80% max weight, so adjusted best glide would be roughly 90% of the published number.I was alone in the plane with 35G fuel. about 500lb under 2550 gross. Not sure on the second part
That would depend on how fast you do your 360.Its good to know how much altitude your airplane loses in a 360 degree turn and what banking to use.
Isn't best glide at the lowest point on the L/D curve? Or is that max endurance? Dang! Math is hard.