2026-09-21T13:49:37Z https://www.ideals.illinois.edu/oai-pmh

oai:www.ideals.illinois.edu:2142/83999 2023-07-11 col_2142_5131 col_2142_14787 com_2142_5130 com_2142_9630 com_2142_234

Bragg, Michael B. Broeren, Andy Paul 2015-09-25T21:13:05Z 2015-09-25T21:13:05Z 10000-01-01 2000 2000 The remaining six airfoils did not exhibit low-frequency unsteady behavior near stall and the resulting lift fluctuations were very small (less than 0.040). These airfoils exhibited trailing-edge separation which moved forward on the airfoil as the angle of attack was increased into stall. The separation was not uniform along the span and the surface flowfield was indicative of stall-cell structures observed by others. This spanwise variation was also observed in the wake. Made available in DSpace on 2015-09-25T21:13:05Z (GMT). No. of bitstreams: 2 license.txt: 4848 bytes, checksum: 96035ab3f5e1c23cc7138a224ce498bd (MD5) 9955592.pdf: 15582310 bytes, checksum: 4b49bdf31b8f67ae6a720b082bde638e (MD5) Previous issue date: 2000 Embargo set by: Seth Robbins for item 85280 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 325 p. Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 2000. http://hdl.handle.net/2142/83999 (MiAaPQ)AAI9955592 eng Engineering, Aerospace An Experimental Study of Unsteady Flow Over Airfoils Near Stall text Mechanical Engineering Mechanical Engineering University of Illinois at Urbana-Champaign Dissertation Ph.D.