Closed-form lift and moment for Osborne's unsteady thin-airfoil theory.
Author:
Affiliation:
1. Avco Everett Research Laboratory Inc., Everett, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference4 articles.
1. Finite elements for axisymmetric solids under arbitrary loadings with nodes on origin.
2. Unsteady thin-airfoil theory for subsonic flow.
3. Compressible unsteady interactions between blade rows.
4. On the Lift and Circulation of Airfoils in Some Unsteady-Flow Problems
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