Sensitivity Analysis of Unsteady Inviscid Flow Through Turbomachinery Cascades
Author:
Affiliation:
1. Duke University, Durham, North Carolina 27708-0300
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1445
Reference5 articles.
1. Aeroacoustics in Turbomachines and Propellers — Future Research Needs
2. Calculation of unsteady flows in turbomachinery using the linearizedEuler equations
3. 2D Linearized Harmonic Euler Flow Analysis for Flutter and Forced Response
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