|
|
1-1
Stringer-Stiffened Polymer Panel
|
Buckling and Post Buckling
|
Simulating
the shear buckling and associated post buckling failure
behavior of the panel
|
Dade
Huang, Levon Minnetyan “Progressive Fracture of
Stitched Stiffened Composite Shear Panels in The
Postbuckling Range” Journal of Plastics Publication
November 18, 2001.
|
|
|
2-1
PMC Panel under Impact
|
Impact and Post Impact
|
Investigating
the low velocity impact and post impact behaviors
of the PMC panel for Boeing
|
Frank
Abdi, Dade Huang, Mohsen Khatiblou, Chris Chamis.
“Impact, and Tension After Impact of Composite
Launch Space Structure”. Sampe Conference Paper
2001.
|
|
|
2-2
Low Speed Impact of A PMC Panel
|
Impact and Post Impact
|
Simulating
the drop test of a PMC panel
|
1.
D. Huang, F. Abdi, M. Khatiblou “Progressive Failure
Analysis (PFA) and Verification of Composite Test
Panel Under Impact and Compression After Impact
(CAI) Loading Using GENOA”. Alpha STAR Technical
Report to Boeing 12/14/1999.
2. D. Huang, F. A., M. Khatiblou “Progressive Failure
Analysis (PFA) and Verification of Composite Test
Panel Under Impact and Tension After Impact (TAI)
Loading Using GENOA”. Report Boeing Company 12/14/1999.
|
|
Consistent
with both the impact and post impact
compression test results 
|
2-3
Compression after Impact of A PMC Panel
|
Impact and Post Impact
|
Simulating
1) the impact response and 2) the failure process
of the subsequent compression with damage inherited
from the impact.
|
1.
Dade Huang, Frank Abdi, Mohsen Khatiblou “Progressive
Failure Analysis (PFA) and Verification of Composite
Test Panel Under Impact and Compression After
Impact (CAI) Loading Using GENOA”. Alpha STAR
Technical Report to Boeing 12/14/1999.
2.
Jay Qian “Progressive Failure Analysis of Composite
Test Panel Under Impact and Compression After
Impact (CAI) Loading (Impact Was Analyzed Using
GENOA’s Progressive Dynamic Failure Analysis Module)”.
|
|
|
3-1
Army PMC Mobile Bridge
|
Fatigue
|
Assessing
the low cycle fatigue failure of the Army PMC mobile
bridge
|
Frank
Abdi, Zhongyan Qian, and Xiaofeng Su, Ramki Iyer,
Ayman Mosallam “COMPOSITE ARMY BRIDGE UNDER FATIGUE
LOADING”. Sampe 2005 Conference Paper,
|
|
Within 1-5% deviation to test
|
3-2
PMC Panel Fatigue
|
Fatigue
|
Evaluating
the fatigue and associated probabilistic responses
of a PMC panel for ORNL and Delphi
|
M.
Lee, M. Short, Frank Abdi, and J. Qian., “A Math
Based Methodology for Longevity Fatigue Prediction
of 3D Woven Fiber Glass Reinforced Vynle-ester
Composite”. SAE, 2006, Detroit, MI. 06M29-M28 Fatigue.
|
|
Consistent with test
|
3-3
Two Stage Fatigue of PMC Panel
|
Fatigue
|
Simulating
the effect of loading sequence on the PMC fatigue
life for NCC (National Composite Center)
|
Z.
(Jay) Qian, Dade Huang and Frank Abdi, “3D Woven Composite
under Two-Stage Fatigue Loading”. Alpha STAR Technical
Report to NCC (National Composite Center). February12,
2005.
|
|
Test is not available
|
4-1
Vanes Made of 2-D and 3-D CMCs
|
Thermal Fatigue/Aging
|
Evaluating
the fiber architecture effect on CMC vane thermal
aging failure for NAVAIR CMC engine design
|
Xiaofeng
Su, Jonas Sudenas, and Frank Abdi, “Low Cost Three
– Dimensional Reinforced Ceramic Matrix Composites
- Report II” Alpha STAR Technical Report of SBIR Phase
I to Navair. March, 2005
|
|
|
5-1
Center Cracked PMC Panel
|
VCCT and DCZM
|
Simulating
the fracture process of a center cracked PMC panel
using DCZM
|
J.
Masters, “ Translaminar Fracture Toughness of
a Composite Wing Skin Made of Stitched Wrap-Knit
Fabric”, NASA Contractor Report 201728,
1997
|
|
|
5-2
PMC Panel with An Inclined Crack
|
VCCT and DCZM
|
Simulating
the fracture process of a PMC panel with an inclined
crack using DCZM
|
J.
Masters, “ Translaminar Fracture Toughness of
a Composite Wing Skin Made of Stitched Wrap-Knit
Fabric”, NASA Contractor Report 201728,
1997
|
|
|
5-3
Compact Tension PMC Panel
|
VCCT and DCZM
|
Simulating
the fracture process of a compact tension PMC panel
using DCZM
|
J.
Masters, “ Translaminar Fracture Toughness of
a Composite Wing Skin Made of Stitched Wrap-Knit
Fabric”, NASA Contractor Report 201728,
1997
|
|
|
5-4
3-stringer PMC Panel2
|
VCCT and DCZM
|
Deterimining
the fracture behavior of a pre-cracked 3-stringer
PMC panel using DCZM for Boeing ACT program - conforms
to FAA certification requirements
|
D.
Moon, F.Abdi and B. Davis, “Discrete Source Damage
Tolerance Evaluation Of S/Rfi Stiffened Panels”,
SAMPE 1999, Long Beach, CA.
|
|
|
5-5
Polymer Honeycomb Facesheet Push-off2
|
VCCT and DCZM
|
Simulating
honeycomb facesheet delamination in a fracture toughness
determination push-off test designed by NASA-LaRc
using DCZM
|
Thomas
S. Gates, Xiaofeng Su, Frank Abdi, Gregory M.
Odegard, and Helen M. Herring, “Facesheet Delamination
of Composite Sandwich Materials at Cryogenic Temperatures”.
Journal of Composite Science and Technology, 2006
|
|
|
6-1
Polymer Composite Panel
|
Crack Density and PFA
|
Simulating
micro crack development in composite for NASA cryogenic
tank design
|
Xiaofeng
Su, Frank Abdi, J. Andre Lavoie “Prediction of
Micro-crack Densities in Cryogenic IM7/977-2 Propellant
Tanks”. SDM 45.
|
|
|
6-2
Polymer Composite Tank Dome (Quadrant Model)
|
Crack Density and PFA
|
Simulating
micro crack development in composite for NASA cryogenic
tank design
|
Xiaofeng
Su, Frank Abdi, J. Andre Lavoie “Prediction of
Micro-crack Densities in Cryogenic IM7/977-2 Propellant
Tanks”. SDM 45.
|
|
Test result is not available
|
7-1
Filament Winding Tank under Pressure2
|
Probabilistic and PFA
|
Evaluating
the probabilistic response of a filament winding pressured
tank
|
Galib
H. Abumeri, B. Golid “Deterministic And Probabilistic
Durability Analysis Of High Fidelity Filament
Wound Army Bottle Tanks”. Alpha STAR Technical
Presentation to Army Arsenal, Huntsville Alabama,
2006.
|
|
|
8-1
CMC Panel under Salt and Moisture Exposure
|
Environmental Effect and PFA
|
Evaluating
the environmental effect on the CMC stiffness and
strength degradations for Navy
|
Frank
Abdi, Galib Abumeri, George Richardson “Thermal
Aging and Progressive Failure Analysis of an Oxide/Oxide
CMC Coupon Subjected to a Transient Flame Loading”.
Sampe 2005 Conference Paper
|
|
Consistent with test
|
9-1
Sandwich Honeycomb T-joint
|
Honeycomb and PFA
|
Simulating
the failure and load capacity of the X-37 sandwich
honeycomb T-joint
|
“GENOA
Progressive Failure Analysis of Advanced Technology
Demonstrator (ATD-2) Test Article”. Chapter
1, and 5 - Contract No: MOD8GXH-863218W
|
|
|
9-2
Wright-Patterson
Honeycomb Fuselodge
|
Honeycomb and PFA
|
Predicting
the failure process of the Wright-Patterson Honeycomb
Fuselodge
|
1.
F. Abdi, T. Castillo, D. Huang V. Chen, A. DelMundo,
“Virtual Testing Of The X37 Space Vehicle” SAMPE
2002, Long Beach CA.
2.
“GENOA Progressive Failure Analysis of Advanced
Technology Demonstrator (ATD-2) Test Article”.
Chapter 1, and 5 - Contract No: MOD8GXH-863218W
|
|
|
10-1
F22 Polymer Composite Panel
|
Static
|
Capturing
edge effect in F22 composite panel under tension
|
N.
J. Pagano, G. A. Schoppner, R. Kim, and F. L.
Abrams, “Steady-State Cracking and Edge Effects
in Thermo-Mechanical Transverse Cracking of Cross
Ply Laminate”. Composite Sciences
and Technology, 58(1998)
|
|
|
10-2
Polymer Honeycomb Facesheet Push-off1
|
Static
|
Simulating
honeycomb facesheet delamination in a fracture toughness
determination push-off test designed by NASA-LaRc
using damage mechanics method
|
Thomas
S. Gates, Xiaofeng Su, Frank Abdi, Gregory M.
Odegard, and Helen M. Herring, “Facesheet Delamination
of Composite Sandwich Materials at Cryogenic Temperatures”.
Journal of Composite Science and Technology, 2006
|
|
|
10-3
3-stringer PMC Panel1
|
Static
|
Deterimining
the fracture behavior of a pre-cracked 3-stringer
PMC panel for Boeing ACT program
|
Darwin
Moon, Frank Abdi, Bill Davis “Discrete Source
Damage Tolerance Evaluation Of S/RFI Stiffened
Panels”. Sampe Conference Paper 1999.
|
|
|
10-4
PMC Open Hole Model
|
Static
|
Evaluating
the failure process of notched composite
|
Steve
Hinrichs, “Stitched Composite Wing Allowable and Miscellaneous
Test Coupon Results”, McDonnell Douglas Aerospace
Transport Aircraft – West. Report # MDC96K0215
|
|
|
10-5
3-point Bending of RCC Panel
|
Static
|
Simulating
the RCC panel bending behavior for return to flight
shuttle
|
V. S. Sokolinsky, J. Housner, J.
Surdenas and F. Abdi, “Progressive Failure Analysis
of Shuttle Reinforced Carbon-Carbon Plate Specimens”,
47 AIAA Paper # 1789, 2006.
|
|
Within 4% deviation to test
|
10-6
PMC Bridge Component
|
Static
|
Evaluating
the PMC component load capacity for Schuler – Hiem Bridge Long Beach, CA
|
A. Mossallam, M. Haroun, A. Abdel-Kareem,
H. Elsanadedy, M. Elbahar, F. Abdi “Service and
Ultimate Behavior of the Schuyler Heim Bridge
Hybrid Composite Deck” ICCE Conference Paper July
6, 2002.
|
|
Within 1-5% deviation to test
|
10-7
Navy Composite Joint
|
Static
|
Determining
strength and failure modes of composite joints to
effect improved design for Navy
|
Cody Godines, Frank Abdi, Steve Kiefer,
Keith Kedward “Simplified Analytical Procedure
for Prediction of Fracture Damage in Composite
Structures”. ASTM Conference Paper 3/17/03.
|
|
Within 8% deviation to test
|
11-1
Filament Winding Tank under Pressure1
|
Filament Winding and PFA
|
Evaluating
the capacity of a filament winding pressured tank
|
Galib
H. Abumeri, B. Golid “Deterministic And Probabilistic
Durability Analysis Of High Fidelity Filament
Wound Army Bottle Tanks”. Alpha STAR Technical
Presentation to Army Arsenal, Huntsville Alabama,
2006.
|
Successfully
modeled the three composite systems |
12-1
Composite Mobile Bridge
|
Material and PFA
|
Modeling
the various composite systems and simulating their
mechanical properties
|
Ayman Mosallam, Frank Abdi, and Xiaofeng Su, "Virtual
Testing And Progressive Failure Analysis Of Army Composite Bridge". Sampe SAMPE 2004, Long Beach, CA 2004,
|
