Macgyver
4th Feb 2006, 15:58
Hello everyone,
I can't seem to understand the difference between these two terms. Sometimes, authors use them interchangeable. Other times, authors mention that they are very different terms, but they fail to give a good explanation of the differences between them.
I am also currently reading the classic "Handling The Big Jets." In the book, there were 2 sections on manoeuvarability that I quite don't understand either, and I hope someone can shed some light on them.
1. On pg 167, the author is talking about the problems of high altitude flight. One of the sections deals with "reduced manoeuvarability." The author uses the chart to show how the buffet speed curves shift with altitude, leading to the lower manoeuvarability. I don't understand the curves, and I don't see how increasing altitude is a problem from a manoeuvarability standpoint.
2. On pg 225, the author is talking about manoeuvering the a/c in rough-air conditions. He states, "note the rough air speed does not change with weight but that the maximum altitude does." I did not follow his explanation, and I'm hoping that someone could perhaps explain why weight has an effect here. My guess is that it relates to the acceleration capabilities of the a/c (i.e. kind of like how Va changes with weight)- but in this case, altitude is a part of the relationship, and I don't see how it fits into it (i.e. back to Va, this speed changes with weight, but not with altitude...the rough air speed, however, changes with does not change with weight).
Thanks in advance.
I can't seem to understand the difference between these two terms. Sometimes, authors use them interchangeable. Other times, authors mention that they are very different terms, but they fail to give a good explanation of the differences between them.
I am also currently reading the classic "Handling The Big Jets." In the book, there were 2 sections on manoeuvarability that I quite don't understand either, and I hope someone can shed some light on them.
1. On pg 167, the author is talking about the problems of high altitude flight. One of the sections deals with "reduced manoeuvarability." The author uses the chart to show how the buffet speed curves shift with altitude, leading to the lower manoeuvarability. I don't understand the curves, and I don't see how increasing altitude is a problem from a manoeuvarability standpoint.
2. On pg 225, the author is talking about manoeuvering the a/c in rough-air conditions. He states, "note the rough air speed does not change with weight but that the maximum altitude does." I did not follow his explanation, and I'm hoping that someone could perhaps explain why weight has an effect here. My guess is that it relates to the acceleration capabilities of the a/c (i.e. kind of like how Va changes with weight)- but in this case, altitude is a part of the relationship, and I don't see how it fits into it (i.e. back to Va, this speed changes with weight, but not with altitude...the rough air speed, however, changes with does not change with weight).
Thanks in advance.