Add to ORKGThe problem to be addressed in this work is that of modeling nondimensional force and moment aerodynamic coefficients over the entire subsonic envelope. The particular application discussed here is the Z force coefficient for the F-18 High Angle of Attack Research Vehicle (HARV)
The F-18 HARV is a modified F-18 Aircraft which is capable of flying in the post-stall regime in ord...
In this paper a parameter estimation technique is proposed which allows for direct updates to the ae...
A wind tunnel experiment for characterizing the aerodynamic and propulsion forces and moments acting...
This paper discusses a simple technique to identify global models for nonlinear aerodynamic force an...
This paper discusses a simple technique to identify global models for nonlinear aerodynamic force an...
This report discusses a simple technique for identifying global models for nonlinear aerodynamic for...
This report discusses a simple technique for identifying global models for nonlinear aerodynamic for...
Due to the requirement of increased performance and maneuverability, the flight envelope of a modern...
A global nonlinear parametric modeling technique is described and demonstrated. The technique uses m...
A generic model of the aerodynamic coefficients was developed using wind tunnel databases for eight ...
This report describes the global nonlinear aerodynamic modeling using multivariate orthogonal functi...
This report describes the global nonlinear aerodynamic modeling using multivariate orthogonal functi...
A global nonlinear parametric modeling technique is described and demonstrated. The technique uses m...
Basic concepts involved in the mathematical modeling of the aerodynamic response of an aircraft to a...
A method for identifying global aerodynamic models from flight data in an efficient manner is explai...
The F-18 HARV is a modified F-18 Aircraft which is capable of flying in the post-stall regime in ord...
In this paper a parameter estimation technique is proposed which allows for direct updates to the ae...
A wind tunnel experiment for characterizing the aerodynamic and propulsion forces and moments acting...
This paper discusses a simple technique to identify global models for nonlinear aerodynamic force an...
This paper discusses a simple technique to identify global models for nonlinear aerodynamic force an...
This report discusses a simple technique for identifying global models for nonlinear aerodynamic for...
This report discusses a simple technique for identifying global models for nonlinear aerodynamic for...
Due to the requirement of increased performance and maneuverability, the flight envelope of a modern...
A global nonlinear parametric modeling technique is described and demonstrated. The technique uses m...
A generic model of the aerodynamic coefficients was developed using wind tunnel databases for eight ...
This report describes the global nonlinear aerodynamic modeling using multivariate orthogonal functi...
This report describes the global nonlinear aerodynamic modeling using multivariate orthogonal functi...
A global nonlinear parametric modeling technique is described and demonstrated. The technique uses m...
Basic concepts involved in the mathematical modeling of the aerodynamic response of an aircraft to a...
A method for identifying global aerodynamic models from flight data in an efficient manner is explai...
The F-18 HARV is a modified F-18 Aircraft which is capable of flying in the post-stall regime in ord...
In this paper a parameter estimation technique is proposed which allows for direct updates to the ae...
A wind tunnel experiment for characterizing the aerodynamic and propulsion forces and moments acting...