Aerodynamic design and evaluation of an open-nose supersonic drone

The objective of this paper is to investigate the efficiency of a proposed supersonic drone configuration, in terms of drag, ram recovery, and fundamental flight performance factors. Sustainable supersonic cruise at Mach 1.6 is the major segment of the mission profile which affects the overall geome...

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Veröffentlicht in:	Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2022-12, Vol.236 (16), p.3387-3410
Hauptverfasser:	Saheby, Eiman B., Hays, Anthony P., Xing, Shen
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Boundary layers CAD Comparative studies Computer aided design Diffusers Drag Engine inlets Flight characteristics Forebodies Inlet pressure Mathematical models Nose Noses (forebodies) Pressure recovery Supersonic flight Thrust
Online-Zugang:	Volltext
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