Wikiposts
Search
Professional Pilot Training (includes ground studies) A forum for those on the steep path to that coveted professional licence. Whether studying for the written exams, training for the flight tests or building experience here's where you can hang out.

Aerodynamics

Thread Tools
 
Search this Thread
 
Old 18th May 2012, 10:21
  #1 (permalink)  
Thread Starter
 
Join Date: Jun 2010
Location: Belfast
Age: 33
Posts: 98
Likes: 0
Received 0 Likes on 0 Posts
Aerodynamics

Hi
Could someone explain "Mach number compressibility effect on the wing"
Thanks
akafrank07 is offline  
Old 18th May 2012, 11:49
  #2 (permalink)  
 
Join Date: Oct 2000
Location: Bristol
Posts: 461
Likes: 0
Received 0 Likes on 0 Posts
It's a big subject, but here's a starter for 10

For small pressure changes, like you get round aircraft at low speed, air doesn't compress much or change much in density. When greater pressure changes are involved, which come in at speeds over about 300kt TAS or Mach 0.4, the air begins to compress and change density. This gives false readings on the ASI, but equally importantly leads to the formation of shock waves over the wing that affect lift, drag and controlablity

Dick
Dick Whittingham is offline  
Old 28th Jul 2012, 19:34
  #3 (permalink)  
Thread Starter
 
Join Date: Jun 2010
Location: Belfast
Age: 33
Posts: 98
Likes: 0
Received 0 Likes on 0 Posts
Thanks very much for that explaination Dick
akafrank07 is offline  

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



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

Copyright © 2024 MH Sub I, LLC dba Internet Brands. All rights reserved. Use of this site indicates your consent to the Terms of Use.