Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Triangular Wing and Canard with Twin Vertical Tails

The static aerodynamic characteristics of a canard airplane configuration having twin vertical stabilizing surfaces are presented. The model consisted of a wing and canard both of triangular plan form and aspect ratio 2 mounted on a Sears-Haack body of fineness ratio 12.5 and two swept and tapered w...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	Peterson, Victor L.
Format:	Report
Sprache:	eng
Schlagworte:	Aircraft Stability And Control
Online-Zugang:	Volltext bestellen
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