Strain-gage bridges were used to make in-flight measurements of bending moment, shear, and torque loads on a low-aspect-ratio, thin, swept wing having a full depth honeycomb sandwich type structure. Standard regression analysis techniques were employed in the calibration of the strain bridges. Comparison of the measured loads with theoretical loads are included.
Strain-gage bridge calibration and flight loads measurements on a low-aspect-ratio thin wing
1975-10-01
Sonstige
Keine Angabe
Englisch
Strain Gage Calibration of a Complex Wing
AIAA | 1977
|Engineering Index Backfile | 1948
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