Page 8 - Combined_134_OCR
P. 8

FLYING CARS


                                                                                     Parachute tube








                                                                                                       Steering

                                         4 Chrysler Hemi engines
                                         with fuel injection


                                                Fuel cell
                                        Front coil
                                         spring/shock


                                                                                   Transfer gear cases
                               Disc broke
                               Coolant
                                                                     r       Driveline
                               tank
                                                                       Front suspension arms
                                                                    Front transmission




                      Goldenrod                                    teract torque. Fuel injection replaced carburetors to
                                                                   reduce frontal area above engines. Air inlets were atop
                                                                   body instead of in the nose, shortening internal duct­
                      Is Aerodynamic 'Lab'—                        ing with its attendant losses.
                                                                     The nose was tapered in planform and in side view
                      Could Challenge Piston Aircraft              to direct half of the air around the sides instead
                                                                   of over the top, reducing lift to improve traction
                                                                   and stability. Underside wheel fairings extended
                     THE LAND speed record (piston engine) auto, the   downward to reduce interference drag. A slow rise
                      Goldenrod, was the first American car of its type   of underside of body behind front axle at a rate of
                     to use the wind tunnel in its design phase. And it   boundary layer buildup alleviated “choking,” provided
                     brought (in 1965) the record to this country for the   some “pitch down” to further reduce lift.
                     first time since 1928. Builders Bud and Bill Sum­  The underside wheel fairings were also designed
                     mers retained Lockheed aerodynamicist Walter Korff   with “toe-in” to cause underside air to be directed
                      to carry out the aerodynamics of the car. The result:   partly outward.
                     the car achieved the lowest drag coefficient of any
                      4-wheeled surface vehicle (0.1165 Cd); it had a down­  Wind tunnel tests involved “tuft” studies to chart
                     load (negative lift) by the shape of its basic body   airflow paths around the body and locate where air
                     alone, and had high speed stability without adding   separation occurs. Tufts are strands of thread taped
                     horizontal or vertical fins, spoilers or weight (ballast).   in place with upper and lower portions free to
                       Although its record was in the 400 mph range,   bend and flow as directed by tunnel wind. As air
                     Korff believes 500-525 mph is the terminal velocity   flow progresses to rear it becomes increasingly dif­
                     for the Goldenrod on dry salt with a long course.   ficult to avoid separation because of the growth of
                       The car was designed with four-wheel drive for   boundary layer and because body surface tapers
                     increased traction. For gun site steering and safety,   inward.
                      driver is in sling-shot position aft of the rear   To' avoid lift, spoilers were located forward, mak­
                     axle, which provides logical space aft of driver for   ing little difference in download, drag or pitching
                     braking chutes. This made possible a vertical wedge   moment. A larger spoiler just ahead of the front
                     shape for least aft-body air flow disturbance. Center   wheels was more effective, increased drag 49% due
                     of gravity was located on diagonal line 45° forward   to air flow separation over the top.
                     from ground at the midpoint of wheelbase. This pro­  Assuming 10% losses for power train and 2,600
                     vided nearly equal weight on all four wheels for   hp at flywheels, the car nets 2,340 hp at wheel
                     equal traction, reduced need for fin area for direc­  hubs. At 525 mph, wind resistance requires 875 hp
                     tional stability.                             and rolling resistance, 1,502 hp. Thus, 2,377 hp is
                       Frontal area was kept to a minimum by in-line   required at the wheels, a bit more than the actual
                      arrangement of engines, clutches and transmission,   net but absolute terminal velocity can’t be reached
                      a major factor for low wind resistance. Engines were   unless an infinite distance is available in which to
                     back-to-back to rotate in opposing directions to coun­  accelerate.



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