Size-Reduction Techniques for the Determination of Efficient Aeroservoelastic Models-Reference-Cited by-同舟云学术

Size-Reduction Techniques for the Determination of Efficient Aeroservoelastic Models

Published:1992 Issue: Volume: Page:263-295
ISSN:0090-5267
Container-title:Control and Dynamic Systems
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Author:

Karpel Mordechay

Publisher

Elsevier

Reference26 articles.

1. “Aeroelasticity,”;Bisplinghoff,1955

2. “Principles of Aeroelasticity,”;Bisplinghoff,1962

3. “A Doublet-Lattice Method for Calculating Lifting Disturbances of Oscillating Surfaces in Subsonic Flow”;Albano;AIAA J.,1969

4. W. M. Adams Jr., S. H. Tiffany, J. R. Newsom and E. L. Peele, “STABCAR- A Program for Finding Characteristic Roots of Systems Having Transcendental Stability Matrices”, NASA TP-2165 (1984).

5. J. R. Newsom, I. Able and H. J. Dunn, “Application of Two Design Methods for Active Flutter Suppression and Wind-Tunnel Test Results”, NASA TP-1653 (1980).

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