Approximate Calculation of the Static Longitudinal Stability of Airplanes (1926)
NASA Technical Reports Server (NTRS) · leaf 25
Figs.6, 7 & 8. N.A.C.A. Technical Memorandum No.387 ■Mouents with ref. to e.g. (accurate) n t! " 11 leading edge (sim- plified) 8° 12° -12° -& 4-0 QO 40 i + a Fig.6 Koment curves. … Fig.7 Effect of stagger cn the effective angle of attack. ^04 + -'heavy 02+ An;:;le of attack 4 8° 12° -031 • . -p=+30° ^;0o heavy. ^ -oe,Lv P=-30° Fig.3 Course of supplementary noment coefficient produced by various angles of stagger.
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