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Vertical prism disparity in aircraft windshields
American Journal of Optometry and Physiological Optics
|September 1, 1981
Summary
Optical distortion in F/FB-111 aircraft windshields was measured. Varying displacement grading correlated with vertical prism disparity, suggesting a need for maximum disparity limits in military aircraft windshield design.
Area of Science:
- Optics and Vision Science
- Aerospace Engineering
- Human Factors Research
Background:
- Optical distortion in aircraft windshields can impact pilot vision.
- Current quantification methods include displacement grading.
- Potential links between optical distortion and binocular stress are hypothesized.
Purpose of the Study:
- To evaluate the relationship between displacement grading and vertical prism disparity in F/FB-111 aircraft windshields.
- To test the hypothesis that displacement grading magnitudes correlate with vertical prism disparity.
- To inform binocular design specifications for military aircraft windshields.
Main Methods:
- Three F/FB-111 windshields with varying displacement grading values were selected.
- Vertical prism disparity was measured for each windshield.
- Displacement grading technique was employed for quantification.
Main Results:
- A direct correlation was found between displacement grading magnitudes and vertical prism disparity.
- The experimental results supported the initial hypothesis.
- Higher displacement grading values corresponded to greater vertical prism disparity.
Conclusions:
- Varying displacement grading in F/FB-111 windshields directly influences vertical prism disparity.
- Establishing a maximum vertical prism disparity value is crucial for binocular design specifications in military aircraft.
- This research supports the need for stricter optical quality standards in aviation windshields.