This paper describes plans and preliminary results for using the NASA Propulsion Systems Lab (PSL) to experimentally study the fundamental physics of ice-crystal ice accretion. Ice accretion due to the ingestion of ice-crystals is being attributed to numerous jet engine powerloss events. The NASA PSL is an altitude jet-engine test facility which has recently added a capability to inject ice particles into the flow. NASA is evaluating whether this facility, in addition to full-engine and motor-driven-rig tests, can be used for more fundamental iceaccretion studies that simulate the different mixed-phase icing conditions along the core flow passage of a turbo-fan engine compressor. The data from such fundamental accretion tests will be used to help develop and validate models of the accretion process. This paper describes the planned studies at PSL as well as some data from some preliminary testing performed in May 2015. This testing examined how a mixed-phase cloud could be generated at PSL using evaporative cooling in a warmer-than-freezing environment. Parameters such as total water content, plenum humidity, and spray bar air and water temperature were varied producing clouds ranging from fully-liquid to fully glaciated including a variety of mixed-phase conditions. Those conditions, along with a variety of test-section measurements, are presented together with images of observed ice accretions. A noteworthy observation from this testing, and similar to other tests, was that the measured temperature and humidity at the test section changed in such a way that the wet-bulb temperature remained nearly constant.