Page 3 - Combined_141_OCR
P. 3

2

                                                                 crease the test Reynolds number in comparison to that of
                                                                 the very large present day airplanes. For the nonengineers,
                                                                 Reynolds number of automobiles is a scaling relationship
                                                                 of vehicle speed and wheelbase. In addition, a test facility
                                                                 with a very large test section and with very low controlled
                                                                 speed was necessary to test the upcoming vertical and short
                                                                 take-off and landing airplanes. These models would have
                      Fig. 2 - United States Airforce C-5A       high energy air (that is, with ejectors) directed toward the
                                                                 tunnel walls, and that constraint had to be reduced. The
                                                                result of these requirements is a tandem test section wind
                                                                 tunnel shown from the air in Fig. 5. This particular facility
                                                                 is also a very good size for testing automobiles aerodynam-
                                                                ically, and it is the only nongovernment wind tunnel where
                                                                 aerodynamic testing of automobiles can be accomplished
                                                                with low blockage effects. The blockage of a full scale
                                                                car in the forward test section is about 3%, and the top speed
                                                                 is about 115 mph. Speeds obtainable in the downstream test
                                                                section reach 200 mph, but the blockage is up to only
                                                                6-1/2%. In the aircraft industry, this is truly a low speed
                                                                wind tunnel, but it has capabilities of reaching just about
                          Fig. 3 - Lockheed L-1011              the top of the speed range of even the Formula I type racing
                                                                vehicles.



















                                                                           Fig. 4 - Lockheed L-500





























                   Fig. 5 - Low speed wind tunnel
   1   2   3   4   5   6   7