Page 224 - Planning and Design of Airports
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Geometric Design of the Airfield     189




                                             N
                                    NNW              NNE

                             NW                    0.5     NE
                                             0.1
                                        0.1       1.0   0.4
                                             0.4
                                    0.2  0.9     1.2  1.0
                       WNW                                      ENE
                                      0.6           1.6
                                  0.2      1.7  2.4 3.0     0.1
                                    0.6  1.7     5.3  3.1  1.7
                                        3.8       6.8
                         W       0.1 0.4  4.9  8.1  7.1  2.3  1.9  0.2  E
                                        2.7       6.4
                                    0.4  1.5     5.8  3.5
                                  0.1      1.7  3.8     1.9
                                             1.8
                                       0.6          1.9     0.1
                        WSW          0.2  0.8    1.0  1.1       ESE
                                             0.4
                                         0.4      0.1
                                             0.1
                              SW       0.3                  SE
                                    SSW             SSE
                                             S

                 FIGURE 6-8  Wind data in wind rose format.




                   from that used in numbering runways since runway designations are based on
                   the magnetic bearing. As illustrated in Fig. 6-9, a runway oriented on an azimuth
                   to true north of 90° to 270° (N 90° E to S 90° W true bearing) will permit operations
                   90.8 percent of the time with the crosswind components not exceeding 15 mi/h.
                      Should the wind analysis not give the desired wind coverage, the template
                   may then be used to determine the direction of a second runway, a crosswind
                   runway, which would increase the wind coverage to 95 percent. This is done by
                   blocking out the area between the two outer parallel lines for the direction of the
                   primary runway (since this has already been counted in the wind coverage for
                   the primary runway) and rotating the template until the percentages between
                   the outer parallel lines for the remaining area for another direction is maximized.
                   If this is done in this problem it is found that the crosswind runway should be
                   located in an orientation of 12° to 192° (N 12° E to S 12° W true bearing). This
                   will permit an additional wind coverage of 6.2 percent above that provided by
                   the runway oriented 90° to 270° for a total wind coverage for both runways of
                   97.0 percent.
                      Let us say that because of noise-sensitive land uses in the direction of the
                   optimal crosswind runway, a crosswind runway will be located at the airport
                   in the orientation of 30° to 210° direction which results in an additional wind
                   coverage of 5.8 percent. This runway orientation, called runway 3–21, is shown
                   in Fig. 6-10. The total wind coverage for both runways is then 96.6 percent. The
                   total wind coverage for a runway in the orientation of 30° to 210° direction is
                   found to be 84.8 percent from Fig. 6-11. The combined wind coverage of 96.6
                   percent for the use of either runway is shown in Fig. 6-11.
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