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74 PERFORMANCE, STABIU-fY, DYNAMICS, AND CONTROL
Fig. 2-4 Forces acfng on a glider.
Consider a glider fiying in a vertical plane as shown iri Fig. 2.4. Note that, for
gliding flight, y < O. With T : 0, Eqs. (2.7) and (2.8) reduce to the following form:
D+ W sin y - 0 (2.29)
L - W cos y - 0 (2.30)
Kinematic equations as given by Eqs. (2.9) and (2.10) are
x - V cos y (2.31)
h = V sin y (2.32)
Generally, the glide angle y is small so that we have
D+ Wy - 0 (2.33)
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