tspear
En-Route
- Joined
- Dec 10, 2010
- Messages
- 3,603
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Timothy
@Clark1961
Try again. I do like to debate, and I do admit when wrong. I also like to debate both sides of an argument, and in almost all cases I can argue either side. Pick a topic and I can provide examples . Lastly stating opinions without fact is not very interesting to debate.
@denverpilot
I have actually read the whole series, and I have taken it apart with engineers and mathematicians. I did this as part of a debate where I stated repeatedly that the plane stalls at the same speed regardless of altitude, which was based on what I was taught by the first couple of CFIs and also what I read in some literature about angle of attack gauges. I lost. Here was test an engineer CFI had me do with him. Take the Cirrus up with full fuel, and test the stall speed and power requirements at 12K density altitude. Note how much fuel was burned before the test. Record the power and speed. Land, top off the tanks. Fly to 9K, burn off the fuel to get back to same weight as 12K before repeating the stall test. Repeat process at 6K and 3K (I was based around DC, so effectively near sea level).
Was there a difference, yes. Was it substantial, not really. Was it enough for me to notice, yes. Most pilots today are so sloppy in the controls and fly with enough margin it likely does not matter. However, if you fly near the margins of the plane, it does matter.
And in the example, a 20HP difference is a 10% power change in the Cirrus SR20. The less power a plane has, the greater this is likely a factor.
Tim
Try again. I do like to debate, and I do admit when wrong. I also like to debate both sides of an argument, and in almost all cases I can argue either side. Pick a topic and I can provide examples . Lastly stating opinions without fact is not very interesting to debate.
@denverpilot
I have actually read the whole series, and I have taken it apart with engineers and mathematicians. I did this as part of a debate where I stated repeatedly that the plane stalls at the same speed regardless of altitude, which was based on what I was taught by the first couple of CFIs and also what I read in some literature about angle of attack gauges. I lost. Here was test an engineer CFI had me do with him. Take the Cirrus up with full fuel, and test the stall speed and power requirements at 12K density altitude. Note how much fuel was burned before the test. Record the power and speed. Land, top off the tanks. Fly to 9K, burn off the fuel to get back to same weight as 12K before repeating the stall test. Repeat process at 6K and 3K (I was based around DC, so effectively near sea level).
Was there a difference, yes. Was it substantial, not really. Was it enough for me to notice, yes. Most pilots today are so sloppy in the controls and fly with enough margin it likely does not matter. However, if you fly near the margins of the plane, it does matter.
And in the example, a 20HP difference is a 10% power change in the Cirrus SR20. The less power a plane has, the greater this is likely a factor.
Tim