Military Aeroplanes, Simplified, Enlarged; An Explanatory Consideration of Their Characteristics, Performances, Construction, Maintenance, And Operation, Specifically Arranged for the Use of Aviators And Students
The book Military Aeroplanes, Simplified, Enlarged; An Explanatory Consideration of Their Characteristics, Performances, Construction, Maintenance, And Operation, Specifically Arranged for the Use of Aviators And Students was written by author Loening, Grover Cleveland, 1888- Here you can read free online of Military Aeroplanes, Simplified, Enlarged; An Explanatory Consideration of Their Characteristics, Performances, Construction, Maintenance, And Operation, Specifically Arranged for the Use of Aviators And Students book, rate and share your impressions in comments. If you don't know what to write, just answer the question: Why is Military Aeroplanes, Simplified, Enlarged; An Explanatory Consideration of Their Characteristics, Performances, Construction, Maintenance, And Operation, Specifically Arranged for the Use of Aviators And Students a good or bad book?
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Combinations of straight lines and circular arcs, parabolic curves, spirals, and the like, have characteric pressures that differ from each other, but in so small an amount that it is hardly necessary to give them separate consideration — excepting in so far as they are taken up later in studies of aeroplane wing sections. The reversed curve, however, is a distinctive geometrical section, to which attention should be given. These sections, as illustrated in the diagram, have the important prope...rty that the center of pressure continues to move forward as the angle is decreased, the character- istic retrograde movement, as found on circular arcs, being apparently absent. As will be explained later, this retrograde movement tends towards instability, and although the ratio of L/D and L are very greatly reduced, by a reverse curve, it becomes necessary to bear in mind that for aeroplane wing sections the loss in efficiency may be worth whUe, in order to gain in stability. 66 Aerofoils. Only flat and the simplest geometrical sections have been con- sidered here.
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