Search

Notices
Flight Schools and Training Ratings, building hours, airmanship, CFI topics

Rate/Radius of Turn

Thread Tools
 
Search this Thread
 
Old 02-08-2010 | 07:14 AM
  #1  
Thread Starter
Line Holder
 
Joined: Dec 2009
Posts: 32
Likes: 0
Default Rate/Radius of Turn

While studying the FAA's Pilot's Handbook of Aeronautical knowledge, I came across two concepts that I know to be true but I can't explain why.

1. Why does the Rate of turn decrease when airspeed increases?

2. Why does the Radius of turn increase when the airspeed increases?
Reply
Old 02-08-2010 | 08:55 AM
  #2  
Cubdriver's Avatar
Moderator
 
Joined: May 2006
Posts: 6,056
Likes: 0
From: ATP, CFI etc.
Default

You have to get into the math a little bit to understand this one, and it has to do with this equation. I put in some dots spacing.

R = V-squared.....
.....g * tan(theta)

where:

R= radius of turn
g= gravity
V= velocity of airplane (speed)
theta= bank angle (zero is no bank)

So, in a level turn weight must equal gravity, and bank angle is constant as well by definition, then what must happen to R with a change in speed (V)?
Reply
Old 02-08-2010 | 09:13 AM
  #3  
ryan1234's Avatar
Gets Weekends Off
 
Joined: Jun 2008
Posts: 1,398
Likes: 0
From: USAF
Default

Originally Posted by Cubdriver

So, in a level turn weight must equal gravity, and bank angle is constant
That's the constant - increase/decrease load factor and it changes.
Reply
Old 02-08-2010 | 09:25 AM
  #4  
Cubdriver's Avatar
Moderator
 
Joined: May 2006
Posts: 6,056
Likes: 0
From: ATP, CFI etc.
Default

Load factor (L/W) does change with speed in constant bank angle level turns, but it does not affect the turn radius, only speed does.

[edit] "shdw" points out in a later post (#22) that this statement was incorrect. Not sure what I was thinking...

Last edited by Cubdriver; 02-12-2010 at 11:22 AM. Reason: correction
Reply
Old 02-08-2010 | 12:49 PM
  #5  
ryan1234's Avatar
Gets Weekends Off
 
Joined: Jun 2008
Posts: 1,398
Likes: 0
From: USAF
Default

I was under the impression that turn performance was based on radial acceleration (vector sum of load factor and gravity).
Reply
Old 02-08-2010 | 01:41 PM
  #6  
UAL T38 Phlyer's Avatar
Moderate Moderator
 
Joined: Mar 2008
Posts: 5,681
Likes: 0
From: Curator at Static Display
Default Practical Example

Gestrich19:

Here's a practical example for you, as this confused me in ground school, too.

Picture yourself walking down the street. You suddenly see a store you want to go into, and make a sharp turn and go inside.

Now, try doing the same thing, running as fast as you can.

Obviously, the radius is bigger for the runner, and he also takes longer to make the turn. That is radius and rate, respectively.

It confused me in ground school/early flying because I told myself: "But the faster I go, the more 'g' that can be generated!"

True, but it doesn't help. I had this discussion with a student recently, and I proved via the lift formula and turn radius formula that for the same angle of attack, the turn radius is a constant. But that is a different side to this discussion.
Reply
Old 02-08-2010 | 01:47 PM
  #7  
UAL T38 Phlyer's Avatar
Moderate Moderator
 
Joined: Mar 2008
Posts: 5,681
Likes: 0
From: Curator at Static Display
Default Half-Right

Originally Posted by ryan1234
I was under the impression that turn performance was based on radial acceleration (vector sum of load factor and gravity).
Ryan:

The first part of your statement is correct: the horizontal component is what counts for turn performance (assuming you are making a horizontal turn, otherwise, a more general and correct statement would be the component in the direction of turn, such as in a loop, immelmann, split-S, pitchback, or sliceback).

But in the horizontal example, the total vector (or 'g'), which is what you feel, is not the horizontal component. Total is vector addition of horizontal and vertical components. So, your equation should say Load Factor = Horizontal + Vertical.
Reply
Old 02-08-2010 | 01:58 PM
  #8  
USMCFLYR's Avatar
Gets Weekends Off
 
Joined: Mar 2008
Posts: 13,843
Likes: 1
From: FAA 'Flight Check'
Default

Originally Posted by UAL T38 Phlyer
Gestrich19:

Here's a practical example for you, as this confused me in ground school, too.

Picture yourself walking down the street. You suddenly see a store you want to go into, and make a sharp turn and go inside.

Now, try doing the same thing, running as fast as you can.

Obviously, the radius is bigger for the runner, and he also takes longer to make the turn. That is radius and rate, respectively.

It confused me in ground school/early flying because I told myself: "But the faster I go, the more 'g' that can be generated!"

True, but it doesn't help. I had this discussion with a student recently, and I proved via the lift formula and turn radius formula that for the same angle of attack, the turn radius is a constant. But that is a different side to this discussion.
But in the EM diagram there is that one point where turn rate and rdius is optimized - correct? Or have I been out of the loop too long?

USMCFLYR
Reply
Old 02-08-2010 | 02:58 PM
  #9  
ryan1234's Avatar
Gets Weekends Off
 
Joined: Jun 2008
Posts: 1,398
Likes: 0
From: USAF
Default

Originally Posted by USMCFLYR
But in the EM diagram there is that one point where turn rate and rdius is optimized - correct? Or have I been out of the loop too long?

USMCFLYR
Is that the corner speed?
Reply
Old 02-08-2010 | 03:03 PM
  #10  
ryan1234's Avatar
Gets Weekends Off
 
Joined: Jun 2008
Posts: 1,398
Likes: 0
From: USAF
Default

Originally Posted by UAL T38 Phlyer
Ryan:

The first part of your statement is correct: the horizontal component is what counts for turn performance (assuming you are making a horizontal turn, otherwise, a more general and correct statement would be the component in the direction of turn, such as in a loop, immelmann, split-S, pitchback, or sliceback).

But in the horizontal example, the total vector (or 'g'), which is what you feel, is not the horizontal component. Total is vector addition of horizontal and vertical components. So, your equation should say Load Factor = Horizontal + Vertical.
Ok... so does that mean that the vertical (over the top 'egg') will have a more positive turn performance while the horizontal will have more negative turn performance?
Reply
Related Topics
Thread
Thread Starter
Forum
Replies
Last Post
EnglishmaninNY
Technical
12
01-16-2011 12:20 PM
DaRaiders
Cargo
2
01-29-2009 01:19 PM
Pecan
Cargo
0
01-06-2009 12:06 PM
USMCFLYR
Flight Schools and Training
19
09-07-2008 05:36 AM
joel payne
Hangar Talk
0
08-24-2008 12:00 PM

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are On
Pingbacks are On
Refbacks are On



Your Privacy Choices