turn co- ordinator???
Thread Starter
Join Date: Feb 2006
Location: BBB
Age: 44
Posts: 63
Likes: 0
Received 0 Likes
on
0 Posts
turn co- ordinator???
q) an a/c is a left hand turn indicating rate 1 and the ball is to the left indicating a slip.
a) the a/c is turning at less than 3 degrees/sec.
b) the a/c is turning at 3 degrees/second.
.... and y???
cheers!!!
a) the a/c is turning at less than 3 degrees/sec.
b) the a/c is turning at 3 degrees/second.
.... and y???
cheers!!!
Join Date: Oct 2006
Location: Bristol
Posts: 332
Likes: 0
Received 0 Likes
on
0 Posts
you're slipping to the inside of the turn, add rudder pressure into the direction of turn and decrease the angle of bank.
rate one turn 3 degree per second= 2 min 360, can't help but feel that slips going to mess with things.
I'm inclined to go with b) but i''ll get back to you after egypt thing finishes on discovery.
Regards
CR
rate one turn 3 degree per second= 2 min 360, can't help but feel that slips going to mess with things.
I'm inclined to go with b) but i''ll get back to you after egypt thing finishes on discovery.
Regards
CR
Join Date: Oct 2006
Location: Bristol
Posts: 332
Likes: 0
Received 0 Likes
on
0 Posts
okay, back from the discovery marathon, those egyptians, bloody incredible I tell thee.
Anyways, yep, back to the question,
You'll be turning at 3 deg/sec as a result of the aircraft being in a slip, stick your hand out in front of you and bank it left, then yaw it slightly to the right, it'll make sense.
Airspeed wise, to get standard rate turn take the airspeed, knock off the last digit, add 5 and that'll give you the angle of bank (roughly) for a standard rate/rate one turn.
120kts
120 (take off the 0=12)
12+5=17
Bosh, 17 degrees of bank for the standard rate turn.
Up to about 250kts this equation works fine for practical purposes.
Regards
CR
Anyways, yep, back to the question,
You'll be turning at 3 deg/sec as a result of the aircraft being in a slip, stick your hand out in front of you and bank it left, then yaw it slightly to the right, it'll make sense.
Airspeed wise, to get standard rate turn take the airspeed, knock off the last digit, add 5 and that'll give you the angle of bank (roughly) for a standard rate/rate one turn.
120kts
120 (take off the 0=12)
12+5=17
Bosh, 17 degrees of bank for the standard rate turn.
Up to about 250kts this equation works fine for practical purposes.
Regards
CR
Last edited by captain_rossco; 18th Jul 2007 at 09:49.
Thread Starter
Join Date: Feb 2006
Location: BBB
Age: 44
Posts: 63
Likes: 0
Received 0 Likes
on
0 Posts
but!!!
did u just change answers???!!!
coz u got it right the first time.... the book says the answer is that the a/c still turns at 3 degrees /sec ...
i thought that the slip would mess with things too...coz you dont have the right angle of bank for the speed to maintain 3 degrees/sec... right???
coz u got it right the first time.... the book says the answer is that the a/c still turns at 3 degrees /sec ...
i thought that the slip would mess with things too...coz you dont have the right angle of bank for the speed to maintain 3 degrees/sec... right???
Join Date: Oct 2006
Location: Bristol
Posts: 332
Likes: 0
Received 0 Likes
on
0 Posts
Shiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiiii iiiiiiiiiiiiiiiiit, have i got this one wrong? Never mind the angle of bank/airspeed etc, does the a/c still turn at 3 deg/sec, thus slip/skid making no dif?
Regards
CR
Regards
CR
Join Date: Jul 2006
Location: The sunny south coast
Age: 52
Posts: 47
Likes: 0
Received 0 Likes
on
0 Posts
I was taught tas/10+7 as well.
This question has got me digging out the books and writting and not submitting a couple of replies cos I keep changing my mind.
Firstly I came up with the same answer as CR, makes sense when slipping the nose of the ac is outside the turn, then I thought if you were using the turn co-ordinator as your reference for the turn it wouldnt matter because the t/c measures the angular acceleration about the normal axis therefore you would still be changing direction at 3 degrees per sec.
This question has got me digging out the books and writting and not submitting a couple of replies cos I keep changing my mind.
Firstly I came up with the same answer as CR, makes sense when slipping the nose of the ac is outside the turn, then I thought if you were using the turn co-ordinator as your reference for the turn it wouldnt matter because the t/c measures the angular acceleration about the normal axis therefore you would still be changing direction at 3 degrees per sec.
Thread Starter
Join Date: Feb 2006
Location: BBB
Age: 44
Posts: 63
Likes: 0
Received 0 Likes
on
0 Posts
pjillpilot
with you on that logic...
coz u could still be turning at 3 degrees/sec ... and the ball just telling you wether you are in balance or not....
hmmmm??
the book says (b)
coz u could still be turning at 3 degrees/sec ... and the ball just telling you wether you are in balance or not....
hmmmm??
the book says (b)
Join Date: Jan 2007
Location: Dunno ... what day is it?
Posts: 273
Likes: 0
Received 0 Likes
on
0 Posts
Capt Rossco is right.
The aircraft is turning at 3˚ per second. The slip is irrelevant.
The turn co-ordinator is a rate gyro. It only indicates a rate of turn, either yaw or (with less sensitivity) roll. At a constant angle of bank the rate indicated is independent of co-ordination of the turn.
The aircraft is turning at 3˚ per second. The slip is irrelevant.
The turn co-ordinator is a rate gyro. It only indicates a rate of turn, either yaw or (with less sensitivity) roll. At a constant angle of bank the rate indicated is independent of co-ordination of the turn.