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.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
