berkshire
New member
- Jun 8, 2005
- 4,429
I am trying to size a brake cable for a footbrake on an experimental sailplane. Single seat, single landing wheel.
I am tring to figure out what load a pilot CAN exert, arching his back and shoving as hard as he/she can. Since the aircraft is a tail dragger design, if the pilot over does it he/she is likely to put the aircraft up on its nose. The other scenario which bother me more, is wet grass, where the pilot locks the wheel which then skids, and the pilot not realizing this, just shoves harder and harder.
FAR 23 is not very helpful on this: it says: ""Sec. 23.405 Secondary control system.
Secondary controls, such as wheel brakes, spoilers, and tab controls, must be designed for the maximum forces that a pilot is likely to apply to those controls.""
All I can find is rearward stick loads of 167lbs in " 23.397 , and I am thinking that a pilot hauling back on the stick must be producing similar loads to a guy shoving on the brakes. If I double that number to 334lbs would this be adequate?
I am not considering G loads such as the 9g forward loading here, I am considering if it gets that high , the pilot has already hit something.
B.E.
The good engineer does not need to memorize every formula; he just needs to know where he can find them when he needs them. Old professor
I am tring to figure out what load a pilot CAN exert, arching his back and shoving as hard as he/she can. Since the aircraft is a tail dragger design, if the pilot over does it he/she is likely to put the aircraft up on its nose. The other scenario which bother me more, is wet grass, where the pilot locks the wheel which then skids, and the pilot not realizing this, just shoves harder and harder.
FAR 23 is not very helpful on this: it says: ""Sec. 23.405 Secondary control system.
Secondary controls, such as wheel brakes, spoilers, and tab controls, must be designed for the maximum forces that a pilot is likely to apply to those controls.""
All I can find is rearward stick loads of 167lbs in " 23.397 , and I am thinking that a pilot hauling back on the stick must be producing similar loads to a guy shoving on the brakes. If I double that number to 334lbs would this be adequate?
I am not considering G loads such as the 9g forward loading here, I am considering if it gets that high , the pilot has already hit something.
B.E.
The good engineer does not need to memorize every formula; he just needs to know where he can find them when he needs them. Old professor