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CH06_Anderson  7/25/01  8:59 AM  Page 164




                 164  CHAPTER SIX















                                        a            b                 c                 d
                                       Fig. 6.12. What the area rule means to fuselage design.






















                                       Fig.6.13. Two T-38 Talons with fuselage “waist.” (Photo courtesy of the U.S.Air Force.)

                                       d has a waist to compensate for the wings, giving it the same cross-
                                       sectional area as a. Fuselage b has higher wave drag due to the
                                       absence of a waist. Fuselage c has the same wave drag as a and d but
                                       at the cost of a small fuselage everywhere.
                                         The area rule is used in the design of most modern fighter aircraft.
                                       A notable airplane with an obvious use of the area rule is the T38
                                       Talon, shown in Figure 6.13.
                                         In the discussion above, a simplification was made. To illustrate the
                                       area rule we used the cross-sectional area as seen from the front, that
                                       is, the area of a slice perpendicular to the axis of the airplane. In
                                              reality, the cross-sectional area must be held constant along a
                    Eight days after the end of WWI
                                              slice whose angle is a function of the airplane’s design Mach
                    the world speed record was set
                                              number. Illustrating this complicated result is beyond the
                    at 163.06 mi/h (262.36 km/h).
                                              scope of this book.
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