Aerodynamic Model Reduction Through Balanced Realization

Aerodynamic Model Reduction Through Balanced Realization

Information on using incompressible potential flow as a means of reducing the complexity of aerodynamic model reduction is presented. The technique was validated against classical two-dimensional incompressible unsteady results, as well as an aeroelastic flutter boundary calculation.

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Veröffentlicht in:AIAA journal 2004-05, Vol.42 (5), p.1045-1048
Hauptverfasser: Rule, John A, Cox, David E, Clark, Robert L
Format: Artikel
Sprache:eng
Schlagworte:
Aerodynamics
Applied fluid mechanics
Exact sciences and technology
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Mathematical models
Physics
Solid mechanics
Structural and continuum mechanics
Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
Vibrations and mechanical waves
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Zusammenfassung:Information on using incompressible potential flow as a means of reducing the complexity of aerodynamic model reduction is presented. The technique was validated against classical two-dimensional incompressible unsteady results, as well as an aeroelastic flutter boundary calculation.
ISSN:0001-1452
1533-385X
DOI:10.2514/1.9596