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On the uniqueness of the minimum-state representation
E. Nissim
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Keyphrases
Two-degree-of-freedom
100%
State Representation
100%
Indicial Function
100%
Flow Regime
50%
Prediction Method
50%
Computational Fluid Dynamics
50%
Unsteady Aerodynamics
50%
Aeroelastic Response
50%
Aerodynamic Lift
50%
Transonic Flow
50%
Computational Fluid Dynamics Modeling
50%
Flutter Boundary
50%
Airfoil
50%
Superposition Principle
50%
Transonic
50%
Typical Section Model
50%
Indicial Response Function
50%
Aerodynamic Moment
50%
Engineering
Computational Fluid Dynamics
100%
Two Degree of Freedom
100%
Good Agreement
50%
Flow Regime
50%
Dynamic Method
50%
Aerodynamic Lift
50%
Airfoil
50%
Response Function
50%
Transonic Flow
50%
Superposition Principle
50%