STRUCTURES, STRUCTURAL DYNAMICS,

(1)

A

_Collection

_of

Technical

_Papers

Volume

3 47th

_{AIAA/ASME/ASCE/AHS/ASC}

STRUCTURES,

STRUCTURAL

_DYNAMICS,

AND

_{MATERIALS CONFERENCE}

14th

_AIAAASME/AHS

_Adaptive

_{Structures Conference}

8th

AIAA

_{Non-Deterministic}

_Approaches

_Conference

7th AiAA

_Gossamer

_Spacecraft

_Forum

2nd AIAA

_{Multidisciplinary}

_Design

_Optimization

Specialist

Conference

NEWPORT,

RHODE ISLAND

1-4

_May

2006

(2)

AIAA-2006-1710 Multilevel Hierarchical

_{Decomposition:}

Identification Procedures for

_Edge

of

_{Design Space Feasibility}

N.

_Somanath,

J.

_Staubach,

and J.

_Midgeley

1465 AIAA-2006-1711 _{Collaborative}

_Optimization

_Framework _Based _on _{the Interaction}

ofLow- and

_{High-Fidelity}

Models and the

_Moving

Least

Squares

Method

P.

_Zadeh,

V.

_Toropov,

and A. Wood 1481

AIAA-2006-1712 Simultaneous Uniform DoEs forModel

_Building

and Validation in the

_{Multidisciplinary Optimization}

Framework

A.

_Narayanan,

V.

_Toropov,

A.

_Wood,

and F.

_Campean

1495 AIAA-2006-1713 Collaboration

_Pursuing

Method

_Using

Latin

_Hypercube

Sampling

D.Wang

1507

AIAA-2006-1714 From Small X to

_Large

X: Assessment of

_{Space-Filling}

Criteria for the

_Design

and

_Analysis

of

_{Computer Experiments}

M.

_Gardner,

V.

_Ramanath,

P.

_{Ayyalasomayajula,}

and A. Patterson 1514 AIAA-2006-1715

_Development

of

_{Repetitive Response}

Surface Enhancement

Technique

for the

_{Multidisciplinary System}

_Optimization

K.

_Jeon,

J.

_Lee,

and Y.

_Byun

1520 AIAA-2006-1716

Optimization

ofa Personnel Launch

System

for

Space

Tourism

Operations

E. Garcia and J.

_Pasqual

1529

AIAA-2006-1717

Development,

Structure, and

_Application

of MAST: A Generic Mission Architecture

_Sizing

Tool

J. Lafleur, C.

_Restrepo,

and M. Grant 1544

AIAA-2006-1718

_{Multidisciplinary Design Optimization}

of

Reentry

Vehicles:

Trajectory

Optimization

and Sensitivities

M. Morand E. Livne 1555

AIAA-2006-1720

Multiobjective

Optimization

of

_Two-Stage

Rockets for Earth-to-Orbit Launch

B. Bairstow, O. de

_Week,

and J. Sobieszczanski-Sobieski 1585

AIAA-2006-1721 Research on

Theory

and

Application

of

Multidisciplinary Design

Optimization

of

_Flying

Vehicles

X.

_Chen,

L. Yan, W. Luo, L

Xu,

Y.

_Zhao,

and Z.

_Wang

1601 AIAA-2006-1722 Mission and

_{System Design}

of

_{Air-Launching}

Rocket

_Using

Multidisciplinary Optimization

Approach

Y.

_Choi,

K. Noh, J.Lee, Y.

_Byun,

and Y. Yu 1625

(3)

AIAA-2006-1725

_{Nonparametric}

RiskAssessment of Gas Turbine

_Engines

M.

_Enright,

C.

_McClung,

and S. Hudak

₁₆₃₃

AIAA-2006-1726 Towards Hardware

_{Implementation}

of a Probabilistic

Fatigue

Algorithm

for

_Engine

Health

_Monitoring

Y.

_Han,

H. Millwater, J.

Portillo,

and E. John

₁₆₄₂

AIAA-2006-1728 Simulation and Classification of Random

_Multiphase

Materials

Through Short-Range

Correlation

L.

_Graham-Brady

and X. Xu 1666 AIAA-2006-1729 Statistical

_Analysis

of Effect of Surface Profile on

Fretting

Fatigue

Life for Ti-6AL-4V

S. Kumari andT. Farris 1675

AIAA-2006-1730 Flutter of

_{Partially Rigid}

Cantilevered Plates in Axial Flow

R. De

Breuker,

M.

Abdalla,

and Z. Gurdal 1696

AIAA-2006-1731 Aerothermoelastic

_Stability

of

_Composite

Aircraft

_Wings

Subjected

to Heat

_Inputs

G.

Polli,

F.

Mastroddi,

L.

Librescu,

and C.

_DiTrapani

1710 AIAA-2006-1732 Finite Element Time Domain - Modal Formulation for Nonlinear

Flutter of

_Composite

Curved Panels

M. Azzouz and C. Mei 1726

AIAA-2006-1734 Nonlinear Aeroelastic Studies on a

Folding

Wing

Configuration

with

_{Free-Play Hinge Nonlinearity}

D. Lee and P. Chen 1754

AIAA-2006-1736 Aeroelastic

_Analysis

ofan Airfoilwith a

Hysteresis

Non-Linearity

Y. Gu and Z.

_Yang

1776

AIAA-2006-1737

_{Energy-Consistent,}

Galerkin

_Approach

for the Nonlinear

Dynamics

of Beams

_Using

Mixed,

Intrinsic

_Equations

M. Patil and M. Althoff , 1785

AIAA-2006-1739

_Dynamics

ofThin-Walled

_Composite

Aircraft

_{Wings Carrying}

External Stores

L.

_Librescu,

O.

_Song,

and H. Kwon 1794 AIAA-2006-1740 Free Vibration ofa

Three-Layered

Sandwich Beam

Using Theory

and

_Experiment

R.

_Banerjee,

C.

_Cheung,

R.

_Morishima,

M.

_Perera,

and J.

_Njuguna

1808 AIAA-2006-1742 Finite Element

_Analysis

of Beams with Nonlocal Foundations

Y. Lei, M.

Friswell,

and S. Adhikari 1830

(4)

AIAA-2006-1744 _{Accurate Structural}

_Dynamic

_Modeling

_{of the} _{Hunter UAV}

Using

Ground

Vibration

_Testing

J. Kosmatka and A. Valdes 1841

AIAA-2006-1745

_{Dynamic Snap Through}

_{of Thin-Walled} _Structures

_by

_a _Reduced Order Method

A.

_Przekop

and S. Rizzi 1853 AIAA-2006-1746 A Reduction Method for Finite Elements Nonlinear

_Dynamic

Analysis

of Shells

P.

_Tiso,

E.

_Jansen,

and M. Abdalla 1864

AIAA-2006-1747 Modified Generalized

_Alpha

Method for

_{Integrating Governing}

Equations

of

_Very

Flexible Aircraft

C. Shearer and C Cesnik 1877

AIAA-2006-1748

_Component

Effective Modal Mass

A.

_Majed

and E. Henkel , 1898

AIAA-2006-1749 Coons

Patch,

Hermite

_{Interpolation}

and

_High-Order

Finite Elements in Structural

_Dynamics

L. Morino and F. Cetta 1902

AIAA-2006-1750

_Comparison

of

_Damage

Path Predictions for

_Composite

Laminates

_{by Explicit}

and Standard Finite Element

_Analysis

Tools

P.

_Bogert,

A.

_{Satyanarayana,}

and P. Chunchu 1919 AIAA-2006-1751

_Applicaton

of Linear Finite Elements to Finite Strain

_Using

Corotation

C. Rankin 1942

AIAA-2006-1753

_{(Student Paper)}

A New Finite Element for a Shear Deformable

Plate

H. Patel and R.

_Shimpi

1970

AIAA-2006-1754 An

_h-Adaptive

Finite Element

_Technique

for Linear Elastic Fracture Problems

A.

Bisi,

S.

Gopalakrishnan,

and B.

_Dattaguru

, 1985

AIAA-2006-1755

Application

of Artificial Neural Networksto the Simulation of

Progressive

Damage

in

Composite

Laminates

C.

_Deenadayalu,

A.

_{Chattopadhyay,}

and X. Zhou 1998 AIAA-2006-1756 A

_Large

Deflection Model for

Thin,

Rectangular

Plates

Subjected

to Blast

_Loading

J. Florek and H.

_Benaroya

2016

(5)

AIAA-2006-1757

_Experimental

and Finite Element

_Analysis

of Preloaded Bolted Joints Under

_{Impact Loading}

B.

OToole,

K.

_Karpanan,

and M.

_Feghhi

₂₀₂₄

AIAA-2006-1758 A Consistent

_{Configuration}

Formulation

_Involving

Continuum

Damage

Mechanics Based

_{Lagrangian Hydrodynamic}

Computational

Framework for 3D

_High-

and

_Hyp

X.

_Zhou,

D.

_Sha,

and K.Tamma 2033

AIAA-2006-1759 Robust Bird-Strike

_Modeling

Based on ALE Formulation

Using

LS-DYNA

V.

_Goyal,

C.

_Huertas,

J.

Borrero,

and T. Leutwiler 2044

AIAA-2006-1760 Channel Section Short Column with Fixed Ends Under Axial

Impact

Load

H.

_Shoji,

M.

_Minegishi,

and T. Aoki 2062 AIAA-2006-1762 Simulation of

_Landing

Events for an Unconventional UAV

Landing

Gear

_{System Using}

Transient

_Dynamics

_Approach

P.

_Nguyen,

S.

_Mak,

and J. Panza 2077 AIAA-2006-1764 A Review of Classical Fiber

_{Microbuckling Analytical}

Solutions

for use with Elastic

Memory Composites

W.

Francis,

M.

Lake,

and J.

_Mayes

2085 AIAA-2006-1765 Electric Field

_Patterning

of Dielectric Particles in

LiquidPolymers

J.

_Boyd,

J.

Lee,

and C. Seo 2097 AIAA-2006-1766

_Modeling

of the Stress- and

_Magnetic

Field-Induced Variant

Reorientation in MSMAs

B. Kiefer and D.

_Lagoudas

2106

AIAA-2006-1767

_Processing

of

_{Light-Weight Shape Memory Alloys Using}

_Spark

Plasma

_Sintering

G.

_Majkic

and Y. Chen 2121 AIAA-2006-1768

_Dynamic

Behavior of

_{Ferromagnetic Shape Memory Alloys}

S.

_Scoby

and Y. Chen 2126 AIAA-2006-1769

_Properties

ofTi50Ni25Cu25

_Melt-Spun

Ribbon

Y.

_Tong

and Y. Liu 2130

AIAA-2006-1770 Mechanical Characterization and

_Modeling

of

Isocyanate-Crosslinked Nanostructured Silica

_Aerogels

(6)

AIAA-2006-1771 AIAA-2006-1772 AIAA-2006-1774 AIAA-2006-1775 AIAA-2006-1776

AIAA-2006-1778

AIAA-2006-1779 AIAA-2006-1780 AIAA-2006-1781 AIAA-2006-1782 AIAA-2006-1783 AIAA-2006-1784

Prediction

of Delamination Resistance in Laminated

Composites

with

_{Electrospun Nano-lnterlayers using}

_a Cohesive Zone Model

S.

_Sinn,

J.

_Park,

R.

_Kim,

W.

_Huh,

and A.

_Roy

2162

Facilitating

Interfacial

_Slip

in Carbon Nanotube

_{Polycarbonate}

Composites

J. _{Suhrand N. Koratkar} ₂₁₇₂

Elastic and Inelastic Behavior ofCarbon Nanotube Reinforced

Polystyrene

D.

_{Krzyzanowski,}

A.

_{Chattopadhyay,}

_{and X. Zhou} ₂₁₇₉

Impact Analysis

of

_{NanoComposites}

A. Avila and H. Duarte 2187

Phonon

_Engineering

of Freeand Embedded Nanocarbon

Fragments:

Heat

_Spreading

and Nanosound

_Propagation

E.

_Glushko,

V.

_Evteev,

N.

_Slusarenko,

I.

_Gurova,

I.

_Tarasov,

and A. Zakhidov ₂₁₉₈

Development

and Verification ofa Probabilistic Model for

_Space

Shuttle Debris

_Transport

B.

_Thacker,

D.

_Riha,

J.

_Pleming,

and L.

_Huyse

2215

Computational

and

_{Analytical Modeling}

of

_Foam,

Ice and Ablator Materials

_Impacting

_Space

Shuttle Thermal Tiles

J.

_Walker,

S.

_Chocron,

and W.

_Gray

2229 Thermal Protection

_{System (TPS)}

_Impact

_Experiments

D.Grosch and F. Bertrand 2242

Progressive

Failure

_Analysis

ofShuttle Reinforced Carbon-Carbon Plate

_Specimens

V.

_Sokolinsky,

J.

Housner,

J.

Surdenas,

and F. Abdi 2255 Fracture Mechanics

_Analysis

of LH2 Feed Line Flow Liners

M.

_James,

D.

_Dawicke,

M.

_Brzowski,

I.

_Raju,

K.

_Elliot,

and C.Harris 2261

A Probabilistic

_{Return-to-Flight}

Assessment of the Orbiter's LH2 Feedline Flowliner

S.

Hudak,

L.

_Huyse,

G.

Chell,

Y.

Lee,

D.

_Riha,

B.

Thacker,

C.

_McClung,

B.

_Gardner,

and J.

_Pleming

2270

Buckling

ofLaminated

_Composite

Platesvia a Refined

Higher-Order

_Theory

L.

Fiedler,

W.

_Lacarbonara,

and F. Vestroni 2286