Page 86 - Planning and Design of Airports
P. 86

58    Airp o r t  Pl anning



                                       Wingspan









                                                Wheel tread or track
                                       Front View

                                        Length


                                                                    Maximum  height



                            Nose                Main gear
                            gear
                             Wheelbase
                                      Side View
                 FIGURE 2-1  Aircraft dimensions.


                 main landing gear. The wheelbase and wheel track of an aircraft
                 determine its minimum turning radius, which in turn plays a large role
                 in the design of taxiway turnoffs, intersections, and other areas on an
                 airfield which require an aircraft to turn.
                    Turning radii are a function of the nose gear steering angle. The
                 larger the angle, the smaller the radii. From the center of rotation the
                 distances to the various parts of the aircraft, such as the wingtips,
                 the nose, or the tail, result in a number of radii. The largest radius is
                 the most critical from the standpoint of clearance to buildings or
                 adjacent aircraft. The minimum turning radius corresponds to the
                 maximum nose gear steering angle specified by the aircraft manufac-
                 turer. The maximum angles vary from 60° to 80°, although for design
                 purposes a steering angle of approximately 50° is often applied.
                    The turning radius of an aircraft may be expressed using the fol-
                 lowing formula:
                                R      = b tan (90 − b) + t/2          (2-1)
                                 180° turn
                 where b = wheelbase of an aircraft
                       t = wheel track of the aircraft
                       b = maximum steering angle
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