creator An, Xuanhong advisor Williams, David R. The transient lift coe cient for a NACA0009 airfoil with pulsed jet actuation type of active ow control at stall conditions is investigated. The experimental mea- surements show the lift coe cient dependence to a single-pulse with di erent pulse widths and amplitudes. Based on the single-pulse with optimal parameters, multi- pulse and continuous pulse actuation cases are studied, which indicate that the pulse interval is the major factor of the active ow control system capability. Linear and nonlinear model are used to predict the lift coe cient variation for di erent input signals to the actuators. A combined nonlinear model is introduced to predict lift coe cient change due to arbitrary unsteady pitching motion with active ow control. Submitted by Liana Khananashvili (khananashvili@iit.edu) on 2014-12-15T18:59:56Z No. of bitstreams: 2 Xuanhong_An_thesis.pdf: 3798031 bytes, checksum: 673477b6665c8382aedb0c20f07b796f (MD5) Signed Title Page.pdf: 204351 bytes, checksum: e5b2744159e789034098dd755aa1ecb6 (MD5) Made available in DSpace on 2014-12-15T18:59:56Z (GMT). No. of bitstreams: 2 Xuanhong_An_thesis.pdf: 3798031 bytes, checksum: 673477b6665c8382aedb0c20f07b796f (MD5) Signed Title Page.pdf: 204351 bytes, checksum: e5b2744159e789034098dd755aa1ecb6 (MD5) Previous issue date: 2014-07 M.S. in Mechanical and Aerospace Engineering, July 2014 2014 2014-07 http://hdl.handle.net/10560/3353 en Thesis born digital application/pdf In Copyright http://rightsstatements.org/page/InC/1.0/ Restricted Access MMAE / Mechanical, Materials, and Aerospace Engineering Illinois Institute of Technology Affiliated department