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TsAGI Science Journal

ISSN 印刷: 1948-2590
ISSN オンライン: 1948-2604

TsAGI Science Journal

DOI: 10.1615/TsAGISciJ.v40.i6.80
pages 733-742

INVESTIGATION OF THE SONIC BOOM OF THE OBLIQUE WING AIRCRAFT

Kyuchul Cho
Institute of KDC

要約

The characteristics of the lift-drag ratios and sonic boom intensity of the aircraft, consisting of the oblique wing, fuselage, and vertical fin, were investigated at M ∼ 1.2−1.98. The investigation results were compared to the results, obtained for the Tu-144 aircraft, having the same fuselage and fin. The Tu-144 aircraft has the same wing area as the aircraft with the oblique wing.


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