SYMMETRIC AND ANTI-SYMMETRIC WING LOADING DISTRIBUTIONS IT is proposed to work out the span loading distribution and lift and drag coefficients of an unstalled wing in symmetric flight, together with the wing rolling and yawing derivatives for rolling and yawing flight. The only data assumed are a knowledge of the geometry of the wing and of the slope of the lift-incidence curve of any section of the wing when referred to infinite aspect ratio.
The Lateral Stability of Aeroplanes
Derivative Calculation by the Lotz System
Aircraft Engineering and Aerospace Technology ; 15 , 12 ; 345-351
01.12.1943
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Lateral stability of aeroplanes
Engineering Index Backfile | 1943
|Lateral stability in aeroplanes
Engineering Index Backfile | 1918
|The Lateral Stability of Aeroplanes
Emerald Group Publishing | 1943
|The Lateral Stability of Aeroplanes
Emerald Group Publishing | 1943
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Emerald Group Publishing | 1943
|