Abstract
Calculation methodology to determine parameters of maneuvering aircraft in preliminary design under the conditions of uncertainty is proposed. Application of the methodology is demonstrated on the task of calculating the parameters of the aircraft power plant to meet the range requirements for supersonic cruising flight and requirements for subsonic flight mode.
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.
