On the positive side, they have established that airliner windshields are quite resistant to such impacts. I’d like to see some equivalent simulations for helicopter and GA fixed-wing aircraft, since many of those don’t even survive bird strikes..
It's coming my friend and listed near the back of the document:
Page 33
Phase 2 ‐ FY18 ‐ FY19
Study additional manned airframes such as
rotorcraft and general aviation.
Partnership with industry Original Equipment Manufacturer (OEMs) from the peer
review committee (GE, Pratt and Whitney, Rolls Royce, and Honeywell) to define a
representative engine model to further research sUAS engine ingestion.
Conduct additional UAS component tests for various impact conditions (structural
and rotational) as requested during the peer review with OEMS and FAA Chief
Scientific Technical Advisors (CSTAS).
Phase 3 ‐ 4th Quarter FY18 ‐ FY19
Begin Testing of fan blade assembly.
Develop plan and identify assets/partners/parameters/metrics for engine ingestion
testing using out of service engines; Peer review with OEMS and FAA CSTAS.
Phase 4 ‐ FY20
Execute engine ingestion test using out of service engine; Peer review with OEMS and
FAA CSTAS