Box wing longitudinal flight quality evaluation

Sousa, André N.; de Paula, Adson A.; Cruz Ribeiro, Fábio; Cardoso-Ribeiro, Flávio Luiz

doi:10.2514/6.2019-3490

Verlagslink:	https://www.fzt.haw-hamburg.de/pers/Scholz/Airport2030/Airport2030_PRE_DLRK2019_InducedDragOfBoxWings_19-09-30.pdf http://airport2030.ProfScholz.de
Verlagslink DOI:	10.2514/6.2019-3490
Titel:	Box wing longitudinal flight quality evaluation
Sprache:
Autorenschaft:	Sousa, André N. de Paula, Adson A. Cruz Ribeiro, Fábio Cardoso-Ribeiro, Flávio Luiz
Schlagwörter:	Luftfahrt; Aviation; Box Wing Aircraft; Flight Mechanics; Flying Quality; Flight Dynamics; Vortex Lattice Method; VLM
Erscheinungsdatum:	14-Jun-2019
Verlag:	American Institute of Aeronautics and Astronautics
Konferenz:	AIAA Aviation Forum 2019
Zusammenfassung:	The box wing aircraft is an unconventional design that is esteemed to present lower levels of induced drag when compared with the conventional aircraft design. This configuration presents no horizontal tail and two wings swept in opposite directions in a diamond shape. This work presents an investigation of the longitudinal flight qualities characteristics of a box wing aircraft in the preliminary design phase. The longitudinal stability of a box wing aircraft is being compared with a conventional aircraft with the same narrow body and wing area. The investigation of longitudinal stability includes evaluating means for trimming the box wing, short-period and phugoid oscillation analysis.
URI:	http://hdl.handle.net/20.500.12738/10028
Einrichtung:	Department Fahrzeugtechnik und Flugzeugbau Fakultät Technik und Informatik Forschungsgruppe Flugzeugentwurf und -systeme (AERO)
Dokumenttyp:	Präsentation
Sonstige(r) Teilnehmer*In:	Scholz, Dieter
Enthalten in den Sammlungen:	Publications without full text