Page:Aerial Flight - Volume 1 - Aerodynamics - Frederick Lanchester - 1906.djvu/282

$ 181 columns; both Tables IV. and V. being values of $$\beta$$ appropriate to least gliding angle, that is, for $$\gamma =$$ minimum.

Table VI. gives the theoretical values of $$\gamma$$ corresponding to the ascertained values of $$\beta$$, that is to say, this Table represents the theoretical minimum gliding angle for the values of $$\xi$$ employed.