Load assumptions for calculating the strength of airplanes (1930)
NASA Technical Reports Server (NTRS) · leaf 25
N.A.C.A. Technical Memorandum No* 581 38 b) Vertically: … t , chord of combined fin and rudder (or stabilizer and elevator). p , load per unit area with uniform load distribution. Hence M , moment about C.G. corresponding to 9053 and 9056. Fx , area of fin and rudder (or stabilizer and elevator). I , distance of leading edge of empennage from C.G. of…
NASA Technical Reports Server (NTRS)
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