Go Back  PPRuNe Forums > Other Aircrew Forums > Flight Testing
Reload this Page >

Dutch roll simulation


Notices
Flight Testing A forum for test pilots, flight test engineers, observers, telemetry and instrumentation engineers and anybody else involved in the demanding and complex business of testing aeroplanes, helicopters and equipment.

Dutch roll simulation

Old 25th August 2017 | 12:46
  #1 (permalink)  
Thread Starter
25 Anniversary
 
Joined: May 1999
Posts: 1,846
Likes: 4
From: Bristol, England
Dutch roll simulation

I'm about to brief a 3D animator to show dutch roll building up on a typical airliner (probably B737) at high TAS. My question is, with the yaw stabs out, as the dutch roll builds will the control surfaces deflect? My guess is not.
Alex Whittingham is offline  
Reply
Old 25th August 2017 | 14:00
  #2 (permalink)  
 
Joined: Dec 2002
Posts: 2,776
Likes: 350
From: UK
With irreversible power controls they should not, but if the pilot gets in the loop !!
Stick fixed or stick free.

In order for DR to build up, you should have an initial disturbance; atmosphere or pilot ? And then which axis inputs the disturbance.

In case your animator requires some background maths.
https://www.nasa.gov/centers/dryden/...ain_H-2106.pdf

There may be some simple animations on line like this one https://m.youtube.com/watch?v=oLe8ajpGNTs
Perhaps not that accurate - would reversible manual controls move if stick free.

https://m.youtube.com/watch?v=h-RNbdvrgF0

https://m.youtube.com/watch?v=YTGp-hoUZG0

Last edited by safetypee; 25th August 2017 at 14:19.
safetypee is offline  
Reply
Old 25th August 2017 | 19:54
  #3 (permalink)  
Gender Faculty Specialist
 
Joined: Mar 2002
Aviation Qualifications: ATPL
Posts: 2,325
Likes: 432
From: In your head.
Originally Posted by Alex Whittingham
I'm about to brief a 3D animator to show dutch roll building up on a typical airliner (probably B737) at high TAS. My question is, with the yaw stabs out, as the dutch roll builds will the control surfaces deflect? My guess is not.
As part of post C check air tests I'm required to incite a dutch roll with the yaw damper disengaged and then engage it to ensure it damps correctly.

There is no control surface deflection until the YD is engaged.
Chesty Morgan is offline  
Reply
Old 27th August 2017 | 08:30
  #4 (permalink)  
Thread Starter
25 Anniversary
 
Joined: May 1999
Posts: 1,846
Likes: 4
From: Bristol, England
Thank you all, the term yaw stabs may have slipped in from a past on V bombers, sorry, I did of course mean Yaw Damper. I'm rather constrained to the B737 as it is the model used to illustrate Autoflight in the ATPL syllabus. I have done a you tube trawl but surprisingly there doesn't seem to be much illustrating this. Knowing that the max rudder limiter deflection in the high altitude cruise is 5 deg is particularly useful.

I think may well illustrate an induced oscillation, lightly damped with the yaw damper out then recovering rapidly with the yaw damper selected on.
Alex Whittingham is offline  
Reply
Old 27th August 2017 | 15:51
  #5 (permalink)  
 
Joined: Apr 2009
Aviation Qualifications: ATPL
Posts: 1,481
Likes: 489
From: A place in the sun
Chesty Morgan,

It was the same with the VC10 on which the Dutch Roll doubled its amplitude every 15 seconds.
Bergerie1 is offline  
Reply

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 Off
Pingbacks are Off
Refbacks are Off


Thread Tools
Search this Thread

Contact Us - Archive - Advertising - Cookie Policy - Privacy Statement - Terms of Service

Copyright © 2026 MH Sub I, LLC dba Internet Brands. All rights reserved. Use of this site indicates your consent to the Terms of Use.