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                 the pa  C D  r t  fiv  years. In addition, all automotive trade journals and publications


                 will be scrutinized for pertinent articles written within the last five years.

                 A search will also be made in the Central Engineering library to unearth—


                 any   elated work.

                          An evaluation of the information developed during this search will

                 then be made to insure emphasis is placed on the proper parameters during


                 testing. This information should also reveal the latest testing techniques and

                  imulation parameters (i, e. , advantages of moving ground plane over


                   ound board, if any; effects of spinning wheels, vibration effects, etc. ).
                 O '
                 X
                          Second, an economic and feasibility study will            < D  o onducted to determine


                 whether full scale or something less than full scale testing should               C T  D  C  o  onducted.

                 Consideration will be given to test article cost, test complexity, tunnel


                 cost, tunnel availability, and scaling effects. Included in this study will               C T  D  C

                 an investigation of the proper modeling parameters for engine cooling


                  ystem and compartment simulation.

                          Third, it is proposed that a survey of low sp          ed wind tunnels be mad 0

                 to develop candidate facilities. Cost is always a significant parameter in


                 any program, so all available tunnels will be investigated to insure that

                 maximum benefits are derived from dollars expended. Availability, particu-


                 larly with   government owned facilities, is often a critical factor. This

                              will be cleared early in the program. Tunnel operating parameters


                 (temperature, dynamic pressure, velocity, ) will be listed for each
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