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![]() In properly done flight test work, the altitude is held very constant (10 ft) for at least 5 or 10 minutes, no power changes, after you think you are already stable. It takes this long for the speed to stabilize that last 5 kts or so. The data is taken after it is truly stable. Dead smooth air is required. When done this way, it becomes obvious that there is no such thing as a "step". What we percieve as a step is a climb above the desired altitude and then descend to the altitude before reducing power. After 5 or 10 minutes, we "fall off the step" and have to climb and descend again. We conveniently don't count the extra climb or extra power time. Then the real trick is to determine how much power is being produced. In article k.net, Jerry Springer wrote: David O wrote: Big John wrote: Also in cruise you would climb several hundred feet above your cruise altitude and in a shallow descent back to that altitude pick up 10 mph + which the bird would hold if you were careful and held a constant attitude. Was told (bar talk) that was a characteristic of a laminar flow wing???? With all due respect, John, I rather think it is a characteristic of people's ability to fool themselves. For my part, I'll believe that Mustangs and/or Mooneys have a cruise "step" when an organization such as NASA or CAFE documents the phenomena. The following post by Dr. Philip Bridges of the Aerospace Engineering Department at Mississippi State University echoes my sentiments on the subject, http://tinyurl.com/x48p Correct David, there is no such thing as a step. I had not read Dr Bridges before but fully agree with his statements. Jerry |
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