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#12
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snip
Maintaining a constant attitude in the test you describe will require a pitch control input and that input controls what happens to the glider as the devices are deployed. *To put it another way, maintaining pitch attitude is an arbitrary choice. *You could have specified constant sink rate, constant glide path, constant airspeed, etc etc. *That close to the ground my intent is to control sink rate and the controls interact to achieve that. In my experience deploying my top surface devices with stick free results in nose down pitch, increased sink rate, and airspeed remains essentially constant. Who can define the name of the device that causes that? Andy Yes, I specified constant attitude simply because I can obviously stop the descent by pitching back up. I was just trying to Isolate the effects of the various drag devices which as you point out is simlar no matter what the initial steady state is. One other feature I have noticed on Spoilers is they tend to be ON/OFF as opposed to Airbrakes that tend to be more proportional. I.E. in my example if you slowly apply the Spoilers at a certain point the glider will just drop. Where as the Airbrakes will tend to gradually become more effective. Brian |
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