Page 222 - Planning and Design of Airports
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Geometric Design of the Airfield     187



                           N
                    NNW         NNE
                           35
                 NW        25        NE                          15 mi/h
                           20
                           15
              WNW                     ENE
                           4
              W                         E

                                      ESE
              WSW                3.0
                 SW                 SE
                     SSW       SSE
                           S

            FIGURE 6-7  Wind rose coordinate system and template.

                 A typical wind rose polar coordinate system is shown on the left side
                 of Fig. 6-7. The shaded area indicates that the wind comes from the
                 southeast (SE) with a magnitude between 20 and 25 mi/h. A template
                 is also drawn to the same radial scale representing the crosswind
                 component limits. A template drawn with crosswind component lim-
                 its of 15 mi/h is shown on the right side of Fig. 6-7. On this template
                 three equally spaced parallel lines have been plotted. The middle line
                 represents the runway centerline, and the distance between the mid-
                 dle line and each outside line is, to scale, the allowable crosswind
                 component (in this case, 15 mi/h). The template is placed over the
                 wind rose in such a manner that the centerline on the template passes
                 through the center of the wind rose.
                    By overlaying the template on the wind rose and rotating the cen-
                 terline of the template through the origin of the wind rose one may
                 determine the percentage of time a runway in the direction of the
                 centerline of the template can be used such that the crosswind com-
                 ponent does not exceed 15 mi/h. Optimum runway directions can be
                 determined from this wind rose by the use of the template, typically
                 made on a transparent strip of material. With the center of the wind
                 rose as a pivot point, the template is rotated until the sum of the per-
                 centages included between the outer lines is a maximum. If a wind
                 vector from a segment lies outside either outer line on the template
                 for the given direction of the runway, that wind vector must have a
                 crosswind component which exceeds the allowable crosswind com-
                 ponent plotted on the template. When one of the outer lines on the
                 template divides a segment of wind direction, the fractional part is
                 estimated visually to the nearest 0.1 percent. This procedure is consis-
                 tent with the accuracy of the wind data and assumes that the wind
                 percentage within the sector is uniformly distributed within that sector.
                 In practice, it is usually easier to add the percentages contained in the
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