Fuselage for blended-wing-body vehicle

A study toward finding an efficient noncylindrical fuselage configuration for a conceptual blended-wing-body flight vehicle is presented. A simplified two-dimensional beam-column analysis and optimization was used to demonstrate the problem of containing cabin pressure in such flight vehicles. Then...

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Bibliographische Detailangaben

Veröffentlicht in:	Journal of aircraft 2004-07, Vol.41 (4), p.925-930
Hauptverfasser:	Mukhopadhyay, V, Sobieszczanski-Sobieski, J, Kosaka, I, Quinn, G, Vanderplaats, G N
Format:	Artikel
Sprache:	eng
Online-Zugang:	Volltext
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