Introduction to Aircraft Structural Analysis (Elsevier Aerospace Engineering)

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9.7Tension Field Beams 317

Fig.9.17


Determination of plastic hinge position.


Then,

Sxccφ= 2 Mpc′φ+σtctwsin^2 θ

c^2 c
2

φ

TheminimumvalueofSxisobtainedbydifferentiatingwithrespecttocc,thatis,

dSx
dcc

=− 2

Mpc′
c^2 c

+σtctw

sin^2 θ
2

= 0

whichgives


c^2 c=

4 Mpc′
σtctwsin^2 θ

(9.56)

Similarly,inthetensionflange,


c^2 t=

4 Mpt′
σtttwsin^2 θ

(9.57)

Clearly,fortheplastichingestooccurwithinaflange,bothccandctmustbelessthanb.Therefore,
fromEq.(9.56),


Mpc′ <

twb^2 sin^2 θ
4

σtc (9.58)

whereσtcisfoundfromEqs.(9.52)and(9.53)atthemidpointofWX.
TheaverageaxialstressinthecompressionflangebetweenWandXisobtainedbyconsideringthe
equilibriumofhalfofthelengthofWX(Fig.9.18).
Then,


Fc=σcfAcf+σtctw

cc
2

sinθcosθ+τmtw

cc
2
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