Metric half-span model support system
AssigneeThe United States of America as represented by the Administrator of the National Aeronautics and Space Administration
InventorsCharlie M. Jackson, Jr., Samuel M. Dollyhigh, David S. Shaw
Life of this patent
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Abstract
The invention relates to a model support system used to support a model in a wind tunnel test section. The model comprises a metric, or measured, half-span 12 supported by a nonmetric, or nonmeasured half-span 11 which is connected to a sting support 13. Moments and forces acting on the metric half-span 12 are measured without interference from the support system during a wind tunnel test.
Claims3
A wind tunnel model and support system for use in a wind tunnel test section comprising in combination:
- a symmetrical model of an aircraft having wings;
- said symmetrical model comprising a metric half-span and a nonmetric half-span;
- said metric half-span being adjacent to said nonmetric half-span at the plane of symmetry of said model;
- sting support means attached to the wing tip of said nonmetric half-span and adapted for attachment to a wind tunnel test section;
- a strain gauge balance positioned within the fuselage of said symmetrical model and connected to said metric half-span and to said nonmetric half-span;
- said sting support means being disposed parallel to the model plane of symmetry and aft of the strain gauge balance position to thereby minimize airflow interference around the model and avoid affecting said strain gauge balance measurements;
- a sealing gasket positioned between said metric half-span and said nonmetric half-span;
- and
- said gasket creating an airtight interface between said metric half-span and said nonmetric half-span.
A method for supporting a model in a wind tunnel test section which comprises:
- providing a symmetrical model of an aircraft having wings and comprising a metric half-span and a nonmetric half-span;
- providing a strain gauge balance for measuring moments and forces on the model;
- positioning the balance between the metric half-span and the nonmetric half-span;
- positioning a sealing gasket within grooves extending along the perimeters of the insides of the half-spans;
- connecting the metric half-span to the balance so as to maintain the metric half-span adjacent to the nonmetrc half-span thereby creating an airtight seal;
- connecting the nonmetric half-span to the balance;
- attaching the nonmetric half-span to a fixed sting support in the wind tunnel test section such that the sting support does not interfere with aerodynamic air flow around the model during testing;
- and
- measuring the moments and forces acting on the metric half-span during a wind tunnel test.
Dependencies are inferred from the claim text.