A high wing airplane will correct itself (lateral stability) when disturbed because its c.g. is below the c.p. (looking at the plane from it'sits side), according to this forum post and the book below.
So my question is, how does this "pendulum effect" affect a biplane with two centres of pressurelift?
A high wing airplane will correct itself (lateral stability) when disturbed because its c.g. is below the c.p. (looking at the plane from it's side), according to this forum post and the book below.
So my question is, how does this "pendulum effect" affect a biplane with two centres of pressure?
A high wing airplane will correct itself (lateral stability) when disturbed because its c.g. is below the c.p. (looking at the plane from its side), according to this forum post and the book below.
So my question is, how does this "pendulum effect" affect a biplane with two centres of lift?
If aA high wing airplane will correct itself (lateral stability) when disturbed because it'sits c.g. is below the c.p. (looking at the plane from it's side)....according to this , according https://www.pprune.org/private-flying/468590-cg-high-low-wing.htmlto this forum post and thisand the book ⬇below.
So my question is,how how does this "pendulum effect" affect a biplane with two centrecentres of pressurespressure?
If a high wing airplane will correct itself (lateral stability) when disturbed because it's c.g is below the c.p (looking at the plane from it's side)....according to this https://www.pprune.org/private-flying/468590-cg-high-low-wing.html and this book ⬇
So my question is,how does this "pendulum effect" affect a biplane with two centre of pressures?
A high wing airplane will correct itself (lateral stability) when disturbed because its c.g. is below the c.p. (looking at the plane from it's side), according to this forum post and the book below.
So my question is, how does this "pendulum effect" affect a biplane with two centres of pressure?
If a high wing airplane will correct itself (lateral stability) when disturbed because it's c.g is below the c.p (looking at the plane from it's side)....according to this https://www.pprune.org/private-flying/468590-cg-high-low-wing.htmla and https://www.pprune.org/private-flying/468590-cg-high-low-wing.html and this book ⬇
So my question is,how does this "pendulum effect" affect a biplane with two centre of pressures?
If a high wing airplane will correct itself (lateral stability) when disturbed because it's c.g is below the c.p (looking at the plane from it's side)....according to this https://www.pprune.org/private-flying/468590-cg-high-low-wing.htmla and this book ⬇
So my question is,how does this "pendulum effect" affect a biplane with two centre of pressures?
If a high wing airplane will correct itself (lateral stability) when disturbed because it's c.g is below the c.p (looking at the plane from it's side)....according to this https://www.pprune.org/private-flying/468590-cg-high-low-wing.html and this book ⬇
So my question is,how does this "pendulum effect" affect a biplane with two centre of pressures?
