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Here we reduced F-4 and F-16 noise measurements in comparison to a Lighthill's method in which the effective jet diameter and r^(-n) propagation rule was used to scale from lab scale Joshi nozzle curves to compare to full-scale measurements.
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This page is a summary of: Verification of Noise Forecast Capabilities for Application to Full-scale Supersonic-capable Jet Engine Development, June 2014, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2014-3162.
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