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Airplane stability in taxying (1932)

NASA Technical Reports Server (NTRS) · leaf 14

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N.A.C.A. Technical MemorandGun No. 682 Figs. 3,4,5 … 93[a,b,f]=0 go = 0.63 Pig. 3 function <P3 = 0, coefficient of friction f as parameter. .2 .4 .5 .8 1.0 a ■b= 0.326 <+53ra,0.326,f] = 0 Fig, 4 Effect of forwaxd position of landing gear. cpg [a,b,fl = 0 go=0.50; Cjjj= +0.128 Fig. 5 Function go=0, coefficient of friction f as parameter

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