16885J/ESD35J-ct1,2002 and o min maX Using Vo=(2L/paScD)2(2nW/paSCD) /2 ReV2/gn becomes R-2(W/S)gpC W/s=wing loading, an important performance parameter And using n=L/W=pV2SC1/2W oegn/v o-g PooV C /2(W/S For each airplane, W/S set by range, payload, V max Then, for a given airplane Rmin=2(W/s)gPoCL max g Provo CLmax /2(W/s) Higher CL.max gives superior turning performance But does n clmax pv2o CLmax /2(W/s)exceed structural limits16.885J/ESD.35J - Oct 1, 2002 Rmin and Zmax Using V’ = (2L/U’SCL)1/2 = (2nW/U’SCL)1/2 R # V2’/gn becomes R = 2(W/S)/ gU’CL W/S = wing loading, an important performance parameter And using n = L/W = U’V2’SCL/2W Z # gn/ V’= g U’V’ CL/2(W/S) For each airplane, W/S set by range, payload, Vmax. Then, for a given airplane Rmin = 2(W/S)/ gU’CL,max Zmax = g U’V’ CL,max /2(W/S) Higher CL,max gives superior turning performance. But does n CL,max = U’V2’ CL,max/2(W/S) exceed structural limits?