Simulation of Turbomachinery Flows on 10-50 GFLOP TestbedsObjective: To permit overnight turnaround of multistage turbomachinery simulations through the use of scalable parallel architectures in solving the Average-Passage model. The goal in computing these simulations is to yield the overall performance map for a given machine on a daily basis. Approach: Develop a multi-level parallel version of APNASA, which implements the Average-Passage flow model for multistage turbomachinery. The code would initially allow for overnight turnaround of a compressor operating point by utilizing both coarse (inter blade row) and fine grain (intra blade row) parallelism to process multistage simulations. Continued software and hardware improvements will lead to overnight turnaround of an overall performance map. Accomplishment: The code has been used to simulate a wide variety of turbomachinery hardware, including multistage compressors consisting of over a dozen stages. One design exercise involved the simulation of an advanced 11+1/2 stage compressor designed by Pratt and Whitney for their 4000 engine series. Another design effort with the Allison Gas Turbine Engine Company simulated a 14+1/2 stage axial flow compressor. In each case an operating point was able to be simulated within 24 hours using the HPCCP IBM SP2 (babbage). Status/Plans: With an upper bound of 150 user accessible processors, a peak of 4.3 GFLOPS has been achieved when running APNASA on the HPCCP IBM SP2 (babbage). Future plans call for demonstrating 10+ GFLOP performance in under 8 hours turnaround time when simulating a compressor operating point. This could be accomplished through the use of larger testbed systems, such as the 384+ node IBM SP2 system located at the Maui High Performance Computing Center. With the ability to simulate multiple operating points within a several hour time frame, an overall performance map can be realistically computed overnight. Richard Mulac, NYMA, Inc. NASA Lewis Research Center MS 5-9, 21000 Brookpark Road Cleveland, Ohio 44135 (216) 433-5936 mulac@lerc.nasa.gov