Page 198 - Understanding Flight
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CH07_Anderson  7/25/01  9:00 AM  Page 185




                                                                                       Airplane Performance 185





                                   Absolute ceiling


                                 Min. level
                                 flight speed


                       Altitude                          Max. climb rate






                                                      Max. climb angle




                                             Speed
                      Fig.7.8. The minimum flight speed and climb speeds meet at the
                      absolute ceiling.

                        As the airplane climbs, its rate of climb decreases. The  The world altitude record for an
                      military defines the combat ceiling as the altitude where the  airplane was set on August 22,
                      best rate of climb drops to 500 ft/min (150 m/min). For some  1963, at 354,200 ft (107,960 m)
                      small general-aviation airplanes that is not much above the  by an X-15.
                      runway at sea level. The  service ceiling of an airplane is
                      defined by the FAA as the altitude at which the airplane’s best rate of
                      climb drops to 100 ft/min (30 m/min). This is a useful measure of the
                      performance of an airplane. If one flies out of a high airport such as
                      the 10,000-ft (3000-m) airport at Leadville, Colorado, an airplane with
                      a 20,000-ft (6000-m) service ceiling is certainly much more desirable
                      than one with a service ceiling of only 14,000 ft (4200 m). The latter
                      airplane will take much more runway to take off and will climb much
                      more slowly.
                        Let us look at two high-altitude aircraft that have taken two different
                      approaches for the same mission. The first is the U-2 high-altitude
                      reconnaissance airplane, shown in Figure 3.5. The airplane is an
                      updated 1950s design with a service ceiling over 70,000 ft (21,000 m).
                      This airplane has a high aspect ratio wing to increase lift efficiency by
                      minimizing drag and maximizing L/D. Its engines are not powerful
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