Page 160 - Aeronautical Engineer Data Book
P. 160

Aircraft performance     133
                       Stepped cruise
             Climb                 Descent
       Transition to
           climb
                                  Landing from
      Taxi out and                  1500 ft
       take-off to
         1500 ft                   and taxi in
                        Range
                    Mission time and fuel
                    Block time and fuel
      Fig. 9.1  A typical operational profile

      Table 9.1 Operational profile terms
      Take off   Take-off run available: operational length of
               the runway.
               Take-off distance available: length of runway
               including stopway (clear area at the end) and
               clearway (distance from end of stopway to
               the nearest 35 ft high obstruction).
               V s : aircraft stall speed in take-off
               configuration.
               V R : rotate speed.
               V 2 : take-off climb speed at 35 ft clearance
               height.
               V mc : minimum speed for safe control.
               V LOF : Lift off speed: speed as aircraft clears
               the ground.
      Transition  V TRANS : average speed during the
      to climb   acceleration from V LOF  to V 2 .
                : final climb gradient.
      Take-off     c : best climb angle.
      climb    1st segment: first part of climb with
               undercarriage still down.
               2nd segment: part of climb between
               ‘undercarriage up’ and a height above ground
               of 400 ft.
               3rd segment: part of climb between 400 ft
               and 1500 ft.
      Climb from  1st segment: part of climb between
      1500 ft to   1500 ft and 10 000 ft.
      cruise   2nd segment: part of climb from 10 000 ft to
               initial cruise altitude.
               V c : rate of climb.
      Cruise   V T : cruise speed.
      Descent   V mc : speed between cruise and 10 000 ft.
               (See Figure 9.2 for further details.)
      Landing   Approach: from 50 ft height to flare height
               (h f ).
               Flare: deceleration from approach speed (V A )
               to touch down speed V TD .
               Ground roll: comprising the free roll (no
               brakes) and the braked roll to a standstill.
   155   156   157   158   159   160   161   162   163   164   165