NASA-CR-112237-1973 Adhesive-bonded scarf and stepped-lap joints《胶粘剂粘合的嵌接处和阶梯搭接式接头》.pdf
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1、it,J i signifies simply that condi-tion (8) was violated. A negative value of Tav/T p indicates such severethermal mismatch between adherends that the joint will break apart prior toapplication of any mechanical loads.12Provided by IHSNot for ResaleNo reproduction or networking permitted without lic
2、ense from IHS-,-,-The computation of joint strength proceeding from the other end of the jointis effected by simply interchanging the subscripts l and 2 on all affectedquantities. With regard to adherend stiffness imbalance alone, it is alwayspossible to identify from equation (28) that the more cri
3、tical end (1) is thatfor which E_R(Z) .C): 1 - .(54)Cnl- (a/g)This can be differentiated with respect to (a/Z) so thata(Tav/T p) / d(a/C) = 0 whena &(1-_-)Cn(l-_-) =(_c)2e+ ,i+ ETR(1)CT_(1)i + ETR(1)CTHERM(1)i - ETR(1) -(_)Substitution of equation (55) into equation (54) yields, for the minimum(stat
4、onary) value of (Tav/_p)i+ ETR(1)CT_(1)a-tv = ETR(1)+T P(55)a _+ m_(_)CTHmM(_) 1+ - i - ETR(1) - . (56)c (_c)This is evidently consistent with the elastic solution (a/z) = 0 for largeoverlaps and, upon subsequent comparison with the more precisely estimatedjoint strengths, proved to be an extremely
5、close lower bound for all cases ofpractical interest. It is significantly conservative only for very short over-laps small values of (_c) or very brittle adhesives very small values of(yp/Ye). The adhesive shear strain capacity yp is involved in equation(56) implicitly through the extent (a/g) of th
6、e plastic zone. Equation (55)19Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-is solved by iteration to evaluate (a/L) and the result substituted intoequation (56) or (54). Appendix A2 contains a listing of the FORTRAN IYdigital computer program emp
7、loyed to solve equations (55) and (54), togetherwith sample outputs and brief user instructions. The iteration techniqueeventually adopted proved to be quite convergent, after other re-arrangementsof equation (55) demonstrated strongly divergent characteristics.This program in Appendix A2 served to
8、provide the initial estimates of (a/L)and (Tav/_p) in the more precise solution listed in Appendix A3. The sequenceof variables used in the solution is (a/L), (Tav/Tp) and (c/L) after which(_av/_p) is recomputed and the estimate of (a/L) adjusted until convergence isattained. In those cases in which
9、 the critical end is not evident by inspec-tion, the potential bond shear strength is computed from each end of the jointand the lower value adopted. Brief user instructions and sample outputs areincluded in Appendix A3.The analyses above for scarf joints pertain to adhesive shear stresses and itis
10、demonstrated that a small enough scarf angle can always be found to transferthe full adherend strength through the bond with an adequate margin. There is,of course, a potential problem with the adherend strength(s) if the scarf angleSpecifically, one adherend will fail if the scarf angle e is sois t
11、oo small.small thate T/Fu , (57)(where F is the ultimate adherend stress in tension, compression, or shear,Uas appropriate) at the more critical end of the joint (identified by the ad-hesive shear stress analysis). Should this situation arise, the solution isto decrease the adherend stiffness imbala
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