PDA

View Full Version : Aerodynamics


akafrank07
18th May 2012, 10:21
Hi
Could someone explain "Mach number compressibility effect on the wing"
Thanks

Dick Whittingham
18th May 2012, 11:49
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

akafrank07
28th Jul 2012, 19:34
Thanks very much for that explaination Dick :)