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#1
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Greg Esres wrote:
I am using Vs (stall, clean) since the configuration is the same as at Va. Vs1 is normally taken to be the clean stall speed. The meaning of Vs seems a bit more ambiguous. But we're talking the same thing here. How does CAS account for density altitude? With a given CAS, the density altitude is irrelevant. That's the beauty of it. ;-) For a given DA, you could use TAS and get the same results, as long as you're consistent in using TAS for each figure. However, Vs1 is only published as CAS. And there's no point in doing that anyway. Thanks, Greg. The whole purpose of my exercise is to determine the minimum turn radius and maximum rate of turn for a given weight. This is dependent upon air density (hence, density altitude) and true airspeed. What is really interesting to me is, I learned all this stuff 25 years ago, but didn't have the experience to fully understand it as I do now. |
#2
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The whole purpose of my exercise is to determine the minimum turn
radius and maximum rate of turn for a given weight. This is dependent upon air density (hence, density altitude) and true airspeed. Hmmm. Air density doesn't appear in the formulas that I have. Load factor and true airspeed are the only variables. And load factor should be independent of density altitude. What are you doing with air density? |
#3
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Greg Esres wrote:
The whole purpose of my exercise is to determine the minimum turn radius and maximum rate of turn for a given weight. This is dependent upon air density (hence, density altitude) and true airspeed. Hmmm. Air density doesn't appear in the formulas that I have. Load factor and true airspeed are the only variables. And load factor should be independent of density altitude. What are you doing with air density? Trying to figure minimum safe altitudes for recovery from vertical dives at different times of the year under different temperature/humidity conditions. |
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