A conformal mapping analysis of cascade trailing-edge flows

Author:

Sekularac Aleksandar1,Falk Eric1,Jumper Eric1,Haven Brenda2

Affiliation:

1. Notre Dame, Univ., IN

2. U.S. Air Force Academy, Colorado Springs, CO

Publisher

American Institute of Aeronautics and Astronautics

Reference47 articles.

1. Conformal mapping

2. Provided that the unsteady compressible flow-field measured in the stationary reference frame of an axial-flow compressor can be approximated by an incompressible solution in a rotating frame, conformal mapping techniques can be used to provide information regarding compressor flow-field physics. Conformal mappings are useful, as they transform the flow-field around a simple geometry to that of a more complex one, by applying stretching, and/or rotation, between coordinate planes. Ig In such transformations, the C-plane is typically denoted as the simple geometry plane, and is defined by the complex coordinates < = < + iv. Conversely, the z-plane is often denoted as the physical plane, or solution plane, and is de&red by the complex coordinates E = x + ~Y.~O Figure 4: Flow about circular cylinder.

3. AI AA 2000-0229 is shown in Fig. 6, where the mean fre+stream velocity, U, has been subtracted from the computed total velocity. Figure 6 clearly shows areas of higher velocities above, and lower velocities below, the free-stream airfoil (the airfoil is located along v = 0), as dictated by suction-surface acceleration and pressuresurface deceleration.

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Unsteady trailing-edge forcing of an IGV forward of a fan in subsonic flow - Amplitude results;37th Joint Propulsion Conference and Exhibit;2001-07-08

2. Evolution of rotor wake in swirling flow;6th Aeroacoustics Conference and Exhibit;2000-06-12

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