March 30, 2002 at 11:12 pm
On a conventional aircraft pitch is controlled by Elevators moving up or down to rotate the aircraft about it’s lateral axis, while the ailerons rotate it about the Longitudinal axis. Delta winged aircraft don’t have a tailplane, so on the trailing edge of the mainplane flying controls surfaces called ELEVONS (ELEVator+AilerONs)are fitted, these move together to provide pitch control, and in opposite directions to provide roll control. The cockpit controls are exactly the same, movement of the stick fore and aft controls pitch, and left to right controls roll.
KeithMac.
(p.s. The Pictures a Vulcan B.1A of the Waddington Wing Battle of Britain Air Show, RAF Leuchars 1966!)
Attachments:
By: neilly - 1st April 2002 at 07:11
RE: Tech Education 2 – Elevons.
One thing about this forum, if you miss the slightest thing someone WILL notice (I’m pleased to say).
Neilly
By: keithmac - 31st March 2002 at 20:29
RE: Tech Education 2 – Elevons.
There are ALWAYS exceptions!
KeithMac
By: J Scott - 31st March 2002 at 16:02
RE: Tech Education 2 – Elevons.
[updated:LAST EDITED ON 31-03-02 AT 04:03 PM (GMT)]Delta winged aircraft don’t have a tailplane?
http://www.aerospaceweb.org/aircraft/fighter/javelin/javelin_14.jpg
By: J Scott - 31st March 2002 at 15:57
RE: Tech Education 2 – Elevons.
Primary Effect of Elevators:
Pitch
Secondary Effect of Elevators:
Speed
By: kev35 - 30th March 2002 at 23:25
RE: Tech Education 2 – Elevons.
Keep going, I’m still with you!
Kev