![]() |
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 |
#11
|
|||
|
|||
![]()
Bertie the Bunyip wrote:
Dudley Henriques wrote in news ![]() Bertie the Bunyip wrote: Dudley Henriques wrote in news:1dCdnWn- : Bertie the Bunyip wrote: OK, I think I have it. There're (roughly) similar problems with the transonic stuff I fly but for some different reasons. Surely there are some buffet isssues with the ailerons at large displacements as well? Bertie I've not noticed aileron buffet in the 38 even at max deflection. The ailerons are extremely effective on the airplane. About buffet; you actually work high performance jets like the 38 by using the buffet boundary. You can pull the pole and feel the buffet onset in pitch. It's a highly effective warning when maneuvering hard. you're talking mach buffet now, right? not normal flow seperation.. I would have thought you might get buffet problems with large deflections in and around transonic flight. We can, certainly, but our airplanes aren't desingned for supersonic flight, of course.. bertie The buffet limit is actually the subsonic buffet limit and defines the lift limit line for the 38. In other words, below corner speed, you are aerodynamically limited in maneuvering room by the lift limit line which basically means you can pull to the buffet. In effect, the tactical buffet line defines the left side of the T38's flight envelope. Yeh, OK I understand buffet in relation to loading but the control deflections have no effect on the onset of buffet? Is that not why you have a limit when close to mach 1? Bertie The roll restriction is totally unrelated to tac buffet. For all practical purposes you can forget aileron buffet as a problem in the T38. The issue with the roll limit is divergence through inertia roll coupling. In other words, at the q found at .9 Mach and above, max aileron throw will generate a roll rate high enough that the roll axis changes from pure roll and couples either in pitch or with yaw or even both under specific angles of attack as the roll is initiated; and this NEW roll axis is so unstable due to the IYMP that departure is a real possibility. -- Dudley Henriques |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
GPS instead of turn and bank | Danny Deger | Piloting | 52 | February 8th 07 02:03 PM |
X-Wings and Canard Rotor Wings. | Charles Gray | Rotorcraft | 1 | March 22nd 05 12:26 AM |
Bank Check Aviation | Ron R | Piloting | 68 | January 19th 05 01:30 AM |
BREAKING THE BANK | Cribsheet | Piloting | 0 | December 22nd 04 06:27 PM |
key bank | CSA722 | Piloting | 0 | July 14th 03 07:04 AM |