Method for determining drag characteristics of aircraft and system for performing the method
AssigneeThe Boeing Company
InventorMathew L. Rueger
Life of this patent
Estimating the term…
Loading patent…
AssigneeThe Boeing Company
InventorMathew L. Rueger
Estimating the term…
A method for designing aircraft including providing a model of the aircraft and a plurality of sensors mounted on the model. The method further includes positioning the aircraft model in a fluid tunnel at an initial attitude and measuring an initial orientation of the aircraft model while the aircraft model is at the initial attitude using a first tilt sensor of the sensors to create initial orientation information. The method also includes passing fluid over the aircraft model using the fluid tunnel and actively moving the aircraft model from the initial attitude to a subsequent attitude. In addition, the method includes measuring a subsequent orientation of the aircraft model while the aircraft model is at the subsequent attitude using a first orientation sensor of the sensors to create subsequent orientation information.
A method for designing an aircraft comprising:
A process for determining drag characteristics of an object in a fluid tunnel comprising:
A process for determining a resulting orientation of an object comprising:
A system for determining a resulting orientation of an object comprising:
Dependencies are inferred from the claim text.