Introduction to Aircraft Structural Analysis (Elsevier Aerospace Engineering)

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5.6 Flexibility Method 141

Similarly,


(^) y=wl^4


(

11

24 EI

+

1

2 GJ

)

(^) z=wl^4


(

1

6 EI

+

1

2 GJ

)

5.6 FlexibilityMethod...................................................................................


An alternative approach to the solution of statically indeterminate beams and frames is to release
thestructure—thatis,removeredundantmembersorsupports—untilthestructurebecomesstatically
determinate.Thedisplacementofsomepointinthereleasedstructureisthendeterminedby,say,the
unit load method. The actual loads on the structure are removed and unknown forces applied to the
pointswherethestructurehasbeenreleased;thedisplacementatthepointproducedbytheseunknown
forcesmust,fromcompatibility,bethesameasthatinthereleasedstructure.Theunknownforcesare
thenobtained;thisapproachisknownastheflexibilitymethod.


Example 5.8
DeterminetheforcesinthemembersofthetrussshowninFig.5.20(a);thecross-sectionalareaAand
Young’smodulusEarethesameforallmembers.


The truss in Fig. 5.20(a) is clearly externally statically determinate but has a degree of internal
staticalindeterminacyequalto1.Wethereforereleasethetrusssothatitbecomesstaticallydeterminate
by“cutting”oneofthemembers,sayBD,asshowninFig.5.20(b).Becauseoftheactualloads(Pin
thiscase),thecutendsofthememberBDwillseparateorcometogether,dependingonwhetherthe
forceinthemember(beforeitwascut)wastensileorcompressive;weshallassumethatitwastensile.


Fig.5.20


Analysis of a statically indeterminate truss.

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