![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
|
#1
|
|||
|
|||
![]() "Marian Aldenhövel" wrote in message ... Hi, I have noticed that most if not all modern gliders are built with a T-Tail (not sure about the term, I am talking about the elevator being located at the top of the tailfin). While most power-aircraft I know right up to the airliners have it at the bottom. It gets the elevator/ horizontal stabilizer up into cleaner air with fewer flow blanking problems from the wing and fuze. Perhaps the biggest advantage is that it gets the stabilizer up high away from damaging obstructions. I have seen one low-down elevator get damaged in ground handling and it was not a pretty sight. Vaughn What are the aerodynamic or constructive reasons for that? Ciao, MM -- Marian Aldenhövel, Rosenhain 23, 53123 Bonn. Fon +49 228 624013, Fax +49 228 624031. http://www.marian-aldenhoevel.de "I know you believe you understand what you think I said, but I'm not sure you realize that what you heard is not what I meant." |
#2
|
|||
|
|||
![]()
All the reasons below are valid.
The reduced interference drag between the vertical and horizontal stab is one of the key factors. Note that the surfaces are aerodynamically off set relative to each other, as well it provides an endplate for the vertical stab. I would venture to say if the conventional tail would give a 1/2 more performance we would still see that type of tail. Never mind ground clearance and other disadvantages. I have noticed that most if not all modern gliders are built with a T-Tail (not sure about the term, I am talking about the elevator being located at the top of the tailfin). While most power-aircraft I know right up to the airliners have it at the bottom. It gets the elevator/ horizontal stabilizer up into cleaner air with fewer flow blanking problems from the wing and fuze. Perhaps the biggest advantage is that it gets the stabilizer up high away from damaging obstructions. I have seen one low-down elevator get damaged in ground handling and it was not a pretty sight. Vaughn What are the aerodynamic or constructive reasons for that? Ciao, MM -- Marian Aldenhvvel, Rosenhain 23, 53123 Bonn. Fon +49 228 624013, Fax +49 228 624031. http://www.marian-aldenhoevel.de "I know you believe you understand what you think I said, but I'm not sure you realize that what you heard is not what I meant." |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Tail Skid Help / Advice | Ray Lovinggood | Soaring | 3 | January 2nd 04 08:16 PM |
AH64 tail rotor | CivetOne | Rotorcraft | 3 | October 23rd 03 07:18 PM |
Oshkosh Get together Roster - Sign in, please! | Bruce E. Butts | Owning | 1 | July 26th 03 11:34 AM |
Oshkosh Get together Roster - Sign in, please! | Bruce E. Butts | Piloting | 1 | July 26th 03 11:34 AM |
The prone postion for tail gunners versus turrets. | The Enlightenment | Military Aviation | 8 | July 22nd 03 11:01 PM |