The uncertainties in real structures usually lead to variations in their dynamic responses. In order to reduce the likelihood of unexpected failures in structures, it is necessary to reduce the response variations. Among various design manipulations, the modification of surface geometry could be a viable option to achieve performance robustness against uncertainties. However, such design modification is difficult to achieve based on conventional finite element methods, primarily due to the inevitable discrepancy between the conventional finite element mesh and the corresponding surface geometry. This issue may become even more severe in design optimization, as an optimized mesh based on conventional finite element analysis may yield nonsmooth surface geometry. In this research, we adopt the nonuniform rational B-splines (NURBS) finite element method to facilitate the robust design optimization (RDO), where the fundamental advantage is that the NURBS finite element mesh is conformal to the underlying NURBS geometry. Furthermore, this conformal feature ensures that, upon finite element-based optimization, the resulting surface geometry is smooth. Taking advantage of that both the uncertainties and the design modifications are small, we formulate a sensitivity-based algorithm to rapidly evaluate the response variations. Based on the direct relation between the response variations and design parameters, the optimal surface geometry that yields the minimal response variation can be identified. Systematic case analyses are carried out to validate the effectiveness and efficiency of the proposed approach.

References

1.
Ashrafiuon
,
H.
,
1993
, “
Design Optimization of Aircraft Engine-Mount Systems
,”
ASME J. Vib. Acoust.
,
115
(
4
), pp.
463
467
.
2.
Kripakaran
,
P.
,
Gupta
,
A.
, and
Baugh
,
J. W.
, Jr.,
2007
, “
A Novel Optimization Approach for Minimum Cost Design of Trusses
,”
Comput. Struct.
,
85
(
23–24
), pp.
1782
1794
.
3.
Sharafi
,
P.
,
Hadi
,
M.
, and
Teh
,
L.
,
2014
, “
Geometric Design Optimization for Dynamic Response Problems of Continuous Reinforced Concrete Beams
,”
J. Comput. Civil Eng.
,
28
(
2
), pp.
202
209
.
4.
Slater
,
J. C.
,
Minkiewicz
,
G. R.
, and
Blair
,
A. J.
,
1999
, “
Forced Response of Bladed Disk Assemblies: A Survey
,”
Shock Vib. Dig.
,
31
(
1
), pp.
17
24
.
5.
Lim
,
S. H.
,
Pierre
,
C.
, and
Castanier
,
M. P.
,
2006
, “
Predicting Blade Stress Levels Directly From Reduced-Order Vibration Models of Mistuned Bladed Disks
,”
ASME J. Turbomach.
,
128
(
1
), pp.
206
210
.
6.
Val
,
D. V.
, and
Stewart
,
M. G.
,
2002
, “
Safety Factors for Assessment of Existing Structures
,”
J. Struct. Eng.
,
128
(
2
), pp.
258
265
.
7.
Lee
,
K.-H.
, and
Park
,
G.-J.
,
2001
, “
Robust Optimization Considering Tolerance of Design Variables
,”
Comput. Struct.
,
79
(
1
), pp.
77
86
.
8.
Doltsinis
,
I.
, and
Kang
,
Z.
,
2004
, “
Robust Design of Structures Using Optimization Methods
,”
Comput. Methods Appl. Mech. Eng.
,
193
(
23–26
), pp.
2221
2237
.
9.
Zang
,
C.
,
Friswell
,
M. I.
, and
Mottershead
,
J. E.
,
2005
, “
A Review of Robust Optimal Design and Its Application in Dynamics
,”
Comput. Struct.
,
83
(
4–5
), pp.
315
326
.
10.
Mohtat
,
A.
, and
Dehghan-Niri
,
E.
,
2011
, “
Generalized Framework for Robust Design of Tuned Mass Damper Systems
,”
J. Sound Vib.
,
330
(
5
), pp.
902
922
.
11.
Youn
,
B. D.
, and
Choi
,
K. K.
,
2004
, “
A New Response Surface Methodology for Reliability-Based Design Optimization
,”
Comput. Struct.
,
82
(
2–3
), pp.
241
256
.
12.
Chiralaksanakul
,
A.
, and
Mahadevan
,
S.
,
2005
, “
First-Order Approximation Methods in Reliability-Based Design Optimization
,”
ASME J. Mech. Des.
,
127
(
5
), pp.
851
857
.
13.
Kodiyalam
,
S.
, and
Parthasarathy
,
V. N.
,
1992
, “
Optimized/Adapted Finite Elements for Structural Shape Optimization
,”
Finite Elem. Anal. Des.
,
12
(
1
), pp.
1
11
.
14.
Le
,
C.
,
Bruns
,
T.
, and
Tortorelli
,
D.
,
2011
, “
A Gradient-Based, Parameter-Free Approach to Shape Optimization
,”
Comput. Methods Appl. Mech. Eng.
,
200
(
9–12
), pp.
985
996
.
15.
Annicchiarico
,
W.
, and
Cerrolaza
,
M.
,
1999
, “
Finite Elements, Genetic Algorithms and B-Splines: A Combined Technique for Shape Optimization
,”
Finite Elem. Anal. Des.
,
33
(
2
), pp.
125
141
.
16.
Zhang
,
Y.
,
Wang
,
W.
, and
Hughes
,
T. J. R.
,
2012
, “
Solid T-Spline Construction From Boundary Representations for Genus-Zero Geometry
,”
Comput. Methods Appl. Mech. Eng.
,
249–252
(
1
), pp.
185
197
.
17.
Hughes
,
T. J. R.
,
Cottrell
,
J. A.
, and
Bazilevs
,
Y.
,
2005
, “
Isogeometric Analysis: CAD, Finite Elements, NURBS, Exact Geometry and Mesh Refinement
,”
Comput. Methods Appl. Mech. Eng.
,
194
(
39–41
), pp.
4135
4195
.
18.
Cottrell
,
A.
,
Reali
,
A.
,
Bazilevs
,
Y.
, and
Hughes
,
T. J. R.
,
2006
, “
Isogeometric Analysis of Structural Vibrations
,”
Comput. Methods Appl. Mech. Eng.
,
195
(
41–43
), pp.
5257
5296
.
19.
Cottrell
,
J. A.
,
Hughes
,
T. J. R.
, and
Bazilevs
,
Y.
,
2009
,
Isogeometric Analysis: Toward Intergration of CAD and FEA
,
Wiley
, Hoboken, NJ.
20.
Hughes
,
T. J. R.
,
Reali
,
A.
, and
Sangalli
,
G.
,
2010
, “
Efficient Quadrature for NURBS-Based Isogeometric Analysis
,”
Comput. Methods Appl. Mech. Eng.
,
199
(
5–8
), pp.
301
313
.
21.
Qian
,
X.
,
2010
, “
Full Analytical Sensitivities in NURBS Based Isogeometric Shape Optimization
,”
Comput. Methods Appl. Mech. Eng.
,
199
(
29–32
), pp.
2059
2071
.
22.
Li
,
K.
, and
Qian
,
X.
,
2011
, “
Isogeometric Analysis and Shape Optimization Via Boundary Integral
,”
Comput. Aided Des.
,
43
(
11
), pp.
1427
1437
.
23.
Zhang
,
O.
, and
Zerva
,
A.
,
1996
, “
Iterative Method for Calculating Derivatives of Eigenvectors
,”
AIAA J.
,
34
(
5
), pp.
1088
1090
.
24.
Leveque
,
R. J.
,
2007
,
Finite Difference Methods for Ordinary and Partial Differential Equations: Steady-State and Time Dependant Problems
,
Society for Industrial and Applied Mathematics
, Philadelphia.
25.
Lee
,
Y. L.
,
Pan
,
J.
,
Hathaway
,
R.
, and
Barkey
,
M.
,
2004
,
Fatigue Testing and Analysis: Theory and Practice
,
Butterworth Heinemann
, Burlington, MA.
26.
Aykan
,
M.
, and
Celik
,
M.
,
2009
,
Vibration Fatigue Analysis and Multi-Axial Effect in Testing of Aerospace Structures
,”
Mech. Syst. Signal Process.
,
23
(
3
), pp.
897
907
.
You do not currently have access to this content.