Vortex-wing interaction of a close-coupled canard configuration

Vortex-wing interaction of a close-coupled canard configuration

The thin-layer Navier Stokes equations are solved numerically to investigate the effects of canard vertical position on a close-coupled, canard-wing-body configuration at a transonic Mach number of 0.9 and angles of attack ranging from negative two to 12 degrees.

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Bibliographische Detailangaben
Veröffentlicht in:Journal of aircraft 1994-03, Vol.31 (2), p.314-321
1. Verfasser: Tu, Eugene L
Format: Artikel
Sprache:eng
Schlagworte:
Aerodynamics
Applied fluid mechanics
Exact sciences and technology
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Military aircraft
Physics
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Beschreibung
Zusammenfassung:The thin-layer Navier Stokes equations are solved numerically to investigate the effects of canard vertical position on a close-coupled, canard-wing-body configuration at a transonic Mach number of 0.9 and angles of attack ranging from negative two to 12 degrees.
ISSN:0021-8669
1533-3868
DOI:10.2514/3.46489