2026-09-21T14:40:26Z https://www.ideals.illinois.edu/oai-pmh

oai:www.ideals.illinois.edu:2142/85067 2023-07-11 col_2142_5131 col_2142_14800 com_2142_5130 com_2142_14799 com_2142_234

Bragg, Michael B. Lee, Sam 2015-09-25T22:34:17Z 2015-09-25T22:34:17Z 10000-01-01 2001 2001 The effects of simulated ice shape on the NLF 0414 were quite different from the NACA 23012m. There was little variation of lift when the simulated ice-shape location was varied from 2% to 20% chord. The large losses in lift occurred when the ice shape was located downstream of 30% chord, and the separation bubble formed over the adverse pressure gradient of the clean airfoil, which started at 75% chord. The effect of the ice shape on the NLF 0414 was not as severe as on the NACA 23012m because the lift was much more aft loaded. Made available in DSpace on 2015-09-25T22:34:17Z (GMT). No. of bitstreams: 2 license.txt: 4848 bytes, checksum: 96035ab3f5e1c23cc7138a224ce498bd (MD5) 3017141.pdf: 10382859 bytes, checksum: 43eb0ab57099b9249992be9b7f534156 (MD5) Previous issue date: 2001 Embargo set by: Seth Robbins for item 86348 Lift date: Forever Reason: Restricted to the U of I community idenfinitely during batch ingest of legacy ETDs Restricted to the U of I community idenfinitely during batch ingest of legacy ETDs U of I Only 288 p. Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 2001. http://hdl.handle.net/2142/85067 (MiAaPQ)AAI3017141 eng Engineering, Aerospace Effects of Supercooled Large -Droplet Icing on Airfoil Aerodynamics text Aerospace Engineering Aerospace Engineering University of Illinois at Urbana-Champaign Dissertation Ph.D.