PSI - Issue 79
D. Marhabi et al. / Procedia Structural Integrity 79 (2026) 34–52
38
(a)
(b)
Figure 1: Rotating bending and line Iso-energy W*
4. OVER-ENERGY IN ELLIPTICAL SECTION WITH THE AXIS , * * a b This part is dedicated to analyze the over-energy expressed in the ellipse support is: RB * , * Rb * W -W W 2 2 2 2 m Rb Rb A Rb Te ds where A y r E R E R
(3)
Or
ds
W
2
2
2 , 1
RB
( , ) W y r dydr Rb
( , ) W y r dydr Rb
*
, 1 Rb
Te
*
Ac
* * Ae b a R R
(4.a)
WTe
A
*
E
2 1
A
RB
R
A c and A e are respectively the circular and the elliptical section (Fig. 1 (1b)) The Integral transformation in elliptical section (Appendix A.1) gives 3 3 2 * * * * 2 2 , 2 ( , ) Rb Rb Eq Rb R a b a b E R R R R A W y u udud e 3 3 2 * * * * 2 2 , 2 ( , ) Rb Rb Eq Rb R a b a b E R R R R W y u udud Ae The Integral transformation in circular section (Appendix A.2) result is: 2 2 2 , 3 2 ( , ) Rb m Rb Rb R E A W y r rdrd c The over-energy (4a) under dissymmetrical rotating bending when * 1 a R
(4.b)
(4.c)
, gives:
3
3
*
*
* * R R a b
a R R b
2
2
2
2
, m Rb 3 ) Rb Rb
(
2
2
, Eq Rb
2
, 1 Te
(5)
, 1
Rb
* * R R b a
E
Rb
2 1 E
For us, this result is necessary to identify threshold stress in the mechanical component. An Asymptotic Method applied to Over-Energy [2] The basic concept in the influence area of no damage crack is expressed by (1.e). We allow writing two limits
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