Last Updated:2025/12/07

The engineers fitted an anti-shock body to the wing to smooth the aircraft's cross-sectional area distribution and reduce wave drag at transonic speeds.

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The engineers fitted an anti-shock body to the wing to smooth the aircraft's cross-sectional area distribution and reduce wave drag at transonic speeds.

音声機能が動作しない場合はこちらをご確認ください
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技術者たちは翼に断面積調整用ポッドを取り付けて機体の断面積分布を滑らかにし、遷音速でのウェーブドラッグを低減した。

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