Title: Aircraft design for flight below the sonic boom speed limit
Abstract: The avoidance of sonic booms places a constraint on aircraft design and can lead to unusual new configurations. From a comparison among several candidate designs, it is shown that an oblique winged aircraft offers many advantages when structure, stability, flight efficiency, and airport noise are considered jointly.
Publication Year: 1974
Publication Date: 1974-05-01
Language: en
Type: article
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Cited By Count: 2
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