This paper introduces a supersonic transport aircraft design model developed in the GENUS aircraft conceptual design environment. A conceptual design model appropriate to supersonic transports with low-to-medium-fidelity methods are developed in GENUS. With this model, the authors reveal the relationship between the sonic boom signature and the lift and volume distributions and the possibility to optimise the lift distribution and volume distribution together so that they can cancel each other at some region. A new inspiring design concept—sonic boom stealth is proposed by the authors. The sonic boom stealth concept is expected to inspire the supersonic aircraft designers to design low-boom concepts through aircraft shaping and to achieve l...
A supersonic airplane creates shocks which coalesce and form a classical N-wave on the ground, formi...
A parametric study of low-boom supersonic transport airplanes with conventional configurations was m...
There exists no publication currently available to the scholars that address in detail, every aspect...
This paper introduces a supersonic aircraft design model developed in a multidisciplinary design ana...
This paper evaluates six supersonic business jet (SSBJ) concepts in a multidisciplinary design analy...
The objective of the sonic boom research in the current High Speed Research Program is to ultimately...
A method for designing conceptual supersonic cruise aircraft to meet low sonic boom requirements is ...
The applicability of sonic boom minimization concepts in the design of large supersonic transport ai...
In this work, the design methodologies and technical rationales for the design of JAXA’s low-boom S4...
This paper evaluates three different class supersonic airliners (Concorde, Cranfield E-5, and NASA Q...
The reduction of sonic boom levels is the main challenge but also the key factor to start a new era ...
The objective of this study was to provide low sonic boom concepts, geometry, and analysis to suppor...
The reduction of sonic boom levels is the main challenge but also the key factor to start a new era ...
This paper introduces a multidisciplinary design analysis and optimization environment called GENUS....
From December 1991 to June 1992, applied aerodynamic research support was given to the team working ...
A supersonic airplane creates shocks which coalesce and form a classical N-wave on the ground, formi...
A parametric study of low-boom supersonic transport airplanes with conventional configurations was m...
There exists no publication currently available to the scholars that address in detail, every aspect...
This paper introduces a supersonic aircraft design model developed in a multidisciplinary design ana...
This paper evaluates six supersonic business jet (SSBJ) concepts in a multidisciplinary design analy...
The objective of the sonic boom research in the current High Speed Research Program is to ultimately...
A method for designing conceptual supersonic cruise aircraft to meet low sonic boom requirements is ...
The applicability of sonic boom minimization concepts in the design of large supersonic transport ai...
In this work, the design methodologies and technical rationales for the design of JAXA’s low-boom S4...
This paper evaluates three different class supersonic airliners (Concorde, Cranfield E-5, and NASA Q...
The reduction of sonic boom levels is the main challenge but also the key factor to start a new era ...
The objective of this study was to provide low sonic boom concepts, geometry, and analysis to suppor...
The reduction of sonic boom levels is the main challenge but also the key factor to start a new era ...
This paper introduces a multidisciplinary design analysis and optimization environment called GENUS....
From December 1991 to June 1992, applied aerodynamic research support was given to the team working ...
A supersonic airplane creates shocks which coalesce and form a classical N-wave on the ground, formi...
A parametric study of low-boom supersonic transport airplanes with conventional configurations was m...
There exists no publication currently available to the scholars that address in detail, every aspect...