This paper documents a process for analyzing whether a particular supersonic aircraft configuration layout and a given cruise condition are feasible to achieve a trimmed low-boom design. This process was motivated by the need to know whether a particular configuration at a given cruise condition could be reshaped to satisfy both low-boom and flight trim constraints. Without such a process, much effort could be wasted on shaping a configuration layout at a cruise condition that could never satisfy both low-boom and flight trim constraints simultaneously. The process helps to exclude infeasible configuration layouts with minimum effort and allows a designer to develop trimmed low-boom concepts more effectively. A notional low-boom supersonic demonstrator concept is used to illustrate the analysis/design process.
Feasibility of Supersonic Aircraft Concepts for Low-Boom and Flight Trim Constraints
AIAA Applied Aerodynamics Conference ; 2015 ; Dallas, TX, United States
2015-06-22
Aufsatz (Konferenz)
Keine Angabe
Englisch
British Library Conference Proceedings | 2015
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