General Theory of the Steady Motion of an Airplane (1921)
NASA Technical Reports Server (NTRS) · leaf 28
ned by equation (59) and the value of y known, it is always possible to correct its value by talking it equal to V -JCos y. For the study of the airplane in steady motion, it is more convenient to consider, instead of the relations (58) and (59), the system of equations p (60) T2 (61) 7 P Jcu which… … the lift coefficient Jcv is a function of the angle of attack only, under the restrictions made, its value can be changed in flight only by a displacement of the control stick. The four quadrants formed' by tw6 straight lines intersecting at right angles will be desig- nated respectively by I, II,…
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