Supplemental data and calculations of the lateral stability of airplanes (1934)
NASA Technical Reports Server (NTRS) · leaf 28
ft.A.C.A. [Technical Mcmorancau.1 No. 742 Figs. 5,6 Figure 5.(example 3).-Theoretical limits of dynamic lateral stability. This figure shows in particular the course of the limit R = 0 (above v. 25° in rough approximation) and location of practical region. Jig. 4c was taken from this. … Figure 6.(example ?).-Li:nits of static lateral stability with given e.g. location (r/t) for three initial conditions (ca), in terms of size of vertical tail surfaces 0Ps/jP) and dihedral (u).
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