![]() |
| 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
|
|||
|
|||
|
Assume you make a glider which is a big cylinder with a huge
hollow tube going through the middle. I lay it on its side and put a clear plexiglass on the top part for the pilot to see out of, and give him a seat inside. Then I put three yawstrings on it: one on the plexiglass "canopy", one in the middle of the center tube, and one on the bottom. I drop this "glider bomb" and it heads straight down (maybe there's a drogue chute). A gyro rotates the cylinder on the way down. Assuming no surface friction and ignoring gyroscopic precession for now, all three yaw strings, from the pilot seat, show different things. If the cylinder is rolling right, the "glider bomb pilot" sees the yawstring on the canopy and instinctively wants to add right rudder. The string in the center of pressure shows straight, and the bottom string would make the pilot want to add left rudder. None of this has anything to do with gravity, adverse yaw, or the cylinder slipping or skidding. I contest that there is an error caused on the yaw string depending on the roll rate, airspeed, and the distance of the yaw string above the center of pressure, and this will always tell the pilot to add more rudder in the direction of roll (assuming the yawstring is above the center of pressure), i.e. skid. The size and importance of this error is another matter entirely :PPP Well, the size and importance DOES matter because you are making such a point of it. I think that I adequately proved that your last point was, shall we say, pointless. The offset of the yaw string to the center of the roll axis is much less than its displacement from the CG, making your "errors" proportionally less. I think you ought to pursue a more reasonable hypothesis; like TWA 800 was downed by a stray Navy missle. Tom |
| Thread Tools | |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| AOPA Stall/Spin Study -- Stowell's Review (8,000 words) | Rich Stowell | Aerobatics | 28 | January 2nd 09 03:26 PM |
| Puchaz Spinning thread that might be of interest in light of the recent accident. | Al | Soaring | 134 | February 9th 04 04:44 PM |
| Puch spin in | Mike Borgelt | Soaring | 18 | January 24th 04 10:29 PM |
| Spinning Horizon | Mike Adams | Owning | 8 | December 26th 03 02:35 AM |
| AOPA Stall/Spin Study -- Stowell's Review (8,000 words) | Rich Stowell | Piloting | 25 | September 11th 03 02:27 PM |