Page 63 - Aeronautical Engineer Data Book
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50      Aeronautical Engineer’s Data Book
      3.3 Densities of liquids at 0°C
      See Table 3.3.
      Table 3.3 Densities of liquids at 0°C

      Liquid        kg/m 3   lb/ft 3   Specific gravity
      Water         1000    62.43    1
      Sea water     1025    63.99    1.025
      Jet fuel  JP 1   800   49.9    0.8
             JP 3    775    48.4     0.775
             JP 4    785    49       0.785
             JP 5    817    51       0.817
      Kerosine       820    51.2     0.82
      Alcohol        801    50       0.801
      Gasoline (petrol)   720   44.9   0.72
      Benzine        899    56.12    0.899
      Oil            890    55.56    0.89


      3.4 Notation: aerodynamics and fluid
      mechanics
      See Table 3.4.
      Table 3.4 Notation: aerodynamics and fluid mechanics
      The complexity of aeronautics means that symbols may
      have several meanings, depending on the context in
      which they are used.
      a     Lift curve slope. Acceleration or deceleration.
            Local speed of sound. Radius of vortex core.
      a'    Inertial or absolute acceleration.
            Speed of sound at sea level. Tailplane zero
      a 0
            incidence lift coefficient.
            Tailplane lift curve slope.
      a 1
            Elevator lift curve slope.
      a 2
            Elevator tab lift curve slope.
      a 3
      a ∞   Lift curve slope of an infinite span wing.
            Local lift curve slope at spanwise co-ordinate h.
      a h
            Local lift curve slope at spanwise co-ordinate y.
      a y
      ac    Aerodynamic centre.
      A     Aspect ratio. Moment of inertia. Area.
      A     State matrix.
      AF    Activity factor of propeller.
      b     Total wing-span (= 2s). Hinge moment
            coefficient slope. Rotational factor in propeller
            theory. General width.
            Elevator hinge moment derivative with respect
      b 1
            to   T .
            Elevator hinge moment derivative with respect to  .
      b 2
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