The Dynamics of the Airplane
The Dynamics of the Airplane
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In our eReader you can find the full English version of the book. Read The Dynamics of the Airplane Online - link to read the book on full screen. Our eReader also allows you to upload and read Pdf, Txt, ePub and fb2 books. In the Mini eReder on the page below you can quickly view all pages of the book - Read Book The Dynamics of the Airplane
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Then since wf(s) Q/S is increasing, and both terms on the right-hand side of the second equation are initially zero, we see from that equation that d must increase. Hence >o. But this evidently contradicts ds the first equation.
36 THE DYNAMICS OF THE AIRPLANE Suppose next that in the interval considered w is decreasing, and therefore negative, since it is initially zero. The second term on the right of the second equation will be >o in the interval, so that we must have tan 0O. There is ds the...refore again a contradiction.
It follows that throughout the interval we must have w = o. Therefore = af(s) It also follows that 6 = constant = tan" 1 -.
We see that the initial conditions that we have assumed are maintained throughout the interval o = s = s', and therefore by a process of continuation will be maintained throughout the motion. Therefore rectilinear motion will assuredly result from the initial conditions and the value of the traction that we have assumed.
What to read after The Dynamics of the Airplane?
You can find similar books in the "Read Also" column, or choose other free books by Kenneth P Kenneth Powers Williams to read onlineMoreLess
To quickly assess the difficulty of the text, read a short excerpt:
Then since wf(s) Q/S is increasing, and both terms on the right-hand side of the second equation are initially zero, we see from that equation that d must increase. Hence >o. But this evidently contradicts ds the first equation.
36 THE DYNAMICS OF THE AIRPLANE Suppose next that in the interval considered w is decreasing, and therefore negative, since it is initially zero. The second term on the right of the second equation will be >o in the interval, so that we must have tan 0O. There is ds the...refore again a contradiction.
It follows that throughout the interval we must have w = o. Therefore = af(s) It also follows that 6 = constant = tan" 1 -.
We see that the initial conditions that we have assumed are maintained throughout the interval o = s = s', and therefore by a process of continuation will be maintained throughout the motion. Therefore rectilinear motion will assuredly result from the initial conditions and the value of the traction that we have assumed.
What to read after The Dynamics of the Airplane?
You can find similar books in the "Read Also" column, or choose other free books by Kenneth P Kenneth Powers Williams to read onlineMoreLess
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