R. Backhouse et P. Ivey, REDUCING COST, TIME AND RISK IN AEROENGINE COMPRESSOR TESTING, Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 211(G6), 1997, pp. 395-402
There is constant pressure to reduce engine development cycles to mini
mize costs and bring forward the revenue earning part of the engine's
life. As cost and time are designed out, the risk of performance short
fall must be minimized by bidding efficiencies from demonstrated techn
ology. This requires a large-scale ongoing advanced development progra
m. In compressor development, high-speed tests are unavoidable but are
expensive; low-speed rigs are easier to instrument and provide a cost
-effective filter for the high-speed designs. The large-scale, low-spe
ed compressor at Cranfield is one of only four worldwide. Recent inves
tment in data reduction software has greatly reduced the test/analysis
cycle time.