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oai:www.ideals.illinois.edu:2142/85132 2023-07-11 col_2142_5131 col_2142_14800 com_2142_5130 com_2142_14799 com_2142_234

Selig, Michael S. Gopalarathnam, Ashok 2015-09-25T22:34:33Z 2015-09-25T22:34:33Z 10000-01-01 1999 1999 In this thesis, the hybrid approach has been applied to the development of inverse methods for the design of (1) multi-element airfoils for multipoint velocity and boundary-layer prescriptions and (2) airfoils to obtain desired multipoint velocity distributions on three-dimensional wings and complex juncture regions. These methods are discussed in detail. Several examples are presented to demonstrate the methods. Finally, the potential of the hybrid design approach for application to the design of other systems such as airfoils with plain flaps and airfoils for wing-fuselage junctures is presented. Made available in DSpace on 2015-09-25T22:34:33Z (GMT). No. of bitstreams: 2 license.txt: 4848 bytes, checksum: 96035ab3f5e1c23cc7138a224ce498bd (MD5) 9953029.pdf: 6456106 bytes, checksum: 1ee828582b81c3b8f43e11d810768664 (MD5) Previous issue date: 1999 Embargo set by: Seth Robbins for item 86413 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 148 p. Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 1999. http://hdl.handle.net/2142/85132 (MiAaPQ)AAI9953029 eng Engineering, Mechanical Hybrid Methods for Inverse Aerodynamic Design text Aerospace Engineering Aerospace Engineering University of Illinois at Urbana-Champaign Dissertation Ph.D.