Introduction to Aircraft Structural Analysis (Elsevier Aerospace Engineering)

(nextflipdebug5) #1
3.4 Torsion of a Narrow Rectangular Strip 79

and
q
N


=−F= 2 G


dz
Theanalogynowbeingestablished,wemaymakeseveralusefuldeductionsrelatingthedeflected
formofthemembranetothestateofstressinthebar.
Contourlinesorlinesofconstantwcorrespondtolinesofconstantφorlinesofshearstressinthe
bar.Theresultantshearstressatanypointistangentialtothemembranecontourlineandequalinvalue
tothenegativeofthemembraneslope,∂w/∂n,atthatpoint,thedirectionnbeingnormaltothecontour
line(seeEq.(3.16)).Thevolumebetweenthemembraneandthexyplaneis


Vol=

∫∫

wdxdy

andweseethatbycomparisonwithEq.(3.8)


T=2Vol

The analogy therefore provides an extremely useful method of analyzing torsion bars possessing
irregular cross sections for which stress function forms are not known. Hetényi [Ref. 2] describes
experimentaltechniquesforthisapproach.Inadditiontothestrictlyexperimentaluseoftheanalogy,it
isalsohelpfulinthevisualappreciationofaparticulartorsionproblem.Thecontourlinesoftenindicate
aformforthestressfunction,enablingasolutiontobeobtainedbythemethodofSection3.1.Stress
concentrationsaremadeapparentbytheclosenessofcontourlines,wheretheslopeofthemembrane
islarge.Theseareinevidenceatsharpinternalcorners,cut-outs,discontinuities,andsoon.


3.4 TorsionofaNarrowRectangularStrip............................................................


InChapter17,weshallinvestigatethetorsionofthin-walledopensectionbeams,thedevelopmentof
thetheorybeingbasedontheanalysisofanarrowrectangularstripsubjectedtotorque.Wenowconve-
nientlyapplythemembraneanalogytothetorsionofsuchastripshowninFig.3.9.Thecorresponding
membrane surface has the same cross-sectional shape at all points along its length except for small
regionsnearitsendswhereitflattensout.Ifweignoretheseregionsandassumethattheshapeofthe
membraneisindependentofy,thenEq.(3.11)simplifiesto


d^2 φ
dx^2

=− 2 G


dz

Integratingtwice


φ=−G


dz

x^2 +Bx+C

Substitutingtheboundaryconditionsφ=0atx=±t/2,wehave


φ=−G


dz

[

x^2 −

(

t
2

) 2 ]

(3.26)
Free download pdf