TsAGI Science Journal
Published 6 issues per year
ISSN Print: 1948-2590
ISSN Online: 1948-2604
INVESTIGATION OF THE SONIC BOOM OF THE OBLIQUE WING AIRCRAFT
Volume 40,
Issue 6, 2009,
pp. 733-742
DOI: 10.1615/TsAGISciJ.v40.i6.80
ABSTRACT
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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