Stress Engineer Mechanical

AL ANH PHAMTUONG

**** ********* *****

Huntington Beach, California 92648

Cellular: 714-***-****

Email: *************@*****.***

OBJECTIVE

Seeking a challenging position as Stress Engineer in load/stress analysis, design, and simulation for development of spacecraft and aircraft composite structures as well as metallic mechanisms.

QUALIFICATIONS SUMMARY

Thirty three years of experience in failure analyses (stress, fatigue, and dynamics) with MSC NASTRAN/PATRAN 2005r3 through 2018 with WordPad on solutions 101, 103, 105, and 106, NASTRAN FEMAP 10.2.0 64-bit finite element modeling for Windows, The Boeing Company’s, United Technology Corp’s., and Northrop Grumman Corp.’s programs in-house developed software, BEAM2D Stress & Deflection Analysis (ORAND Systems), MATHCAD 11, ENOVIA LCA V5 (data base), CATIA V5, UNIGRAPHICS V9 through 13, ANSI Y14.5M, and hand calculations (reference Bruhn, W. Griffel, Roark & Young, Beer & Johnston, and Timoshenko). Education background includes Master Degree of Mechanical Engineering in composite material analysis and design.

PROFESSIONAL EMPLOYMENT

THE BOEING COMPANY, Huntington Beach, California

Metallic and Composite Stress Engineer 2/19 – present Develop metallic and composite interface stress analyses for research and development phase of the Phantom Express space vehicle program on composite nose section using MSC PATRAN/NASTRAN 2018 finite element modeling with Boeing in-house developed software. PANASONIC AVIONICS CORPORATION, Lake Forest, California Metallic and Composite Stress Engineer 11/13 – 2/19 Provide analytical support to current aircraft programs as well as new proposals. Stress and aircraft interface load/stress analyses of In-flight Entertainment/Communication systems on Airbus A-300’s series, Boeing 700’s series, using MSC NASTRAN/PATRAN 2013, and hand calculations.

ANCRA INTERNATIONAL LLC, Azusa, California

Metallic and Composite Stress Engineer 10/12 – 11/13 Provide analytical support to current aircraft programs as well as new proposals. Stress and aircraft interface ground handling plus flight load analyses of Airbus A-300’s series and military A400M, Boeing 767, and DC-10 aircraft cargo and flying hospital systems using NASTRAN FEMAP 10.2.0 64-bit, BEAM2D Stress & Deflection Analysis (ORAND Systems), AutoCAD Mechanical Desktop 2009, and hand calculations. UTC AEROSPACE SYSTEMS, Chula Vista, California

Metallic and Composite Stress Engineer 6/12 – 10/12 Responsible for the Boeing 787-9 program, composite nacelle structures and engine thrust reverser, sections of metallic/composite joints on both hybrid and fabric bond panel using both MSC NASTRAN 2005/PATRAN 2011 64-bit finite element modeling for linear & non-linear solutions 101, 103, 105, and 106 and hand calculations. GOODRICH AEROSTRUCTURES GROUP, Chula Vista, California Metallic and Composite Stress Engineer 7/11 – 6/12 Develop metallic and composite interface stress analyses for certification phase and weight savings of the Airbus A350-XWB program on composite nacelle and engine thrust reverser’s using both MSC NASTRAN 2005/PATRAN 2010.2.3 finite element modeling for linear & non-linear solutions 101, 103, 105, and 106 and hand calculations. NORTHROP GRUMMAN CORPORATION (NGC), El Segundo, California Composite Stress Engineer 9/05 – 10/09

Extract loads from global Finite Element Model (FEM) and build detailed FEM’s to analyze the Joint Strike Fighter F-35 aircraft composite duct panels and lands for static strength, durability

& damage tolerance (D&DT), and buckling & deflection using MSC NASTRAN/PATRAN 2005r3, NGC’s Integrated Detail Analysis Tools (IDAT) software, and hand calculations. Solve MRB’s composite manufacturing issues and interface issues on metallic frames. GOODRICH AEROSTRUCTURES GROUP, Chula Vista, California Load/Stress Engineer 6/05 – 9/05

Develop load/stress analyses to refine new design concepts of composite nacelle and composite/metallic engine thrust reverser for Boeing 787 aircraft by both MSC NASTRAN/PATRAN 2005a finite element modeling and hand calculations. ANCRA INTERNATIONAL LLC, Hawthorne, California

Principal – Engineering Analysis Department 2/99 – 6/05 Responsible for Engineering Analysis Department’s total operation to provide analytical support to all current aircraft programs as well as new proposals. Load, stress and aircraft interface ground handling plus flight load analyses of Airbus A-300’s series, Boeing 737-300, 737 QC, 747-400, 757, 767, MD-11 and DC-10 aircraft cargo systems. SARGENT FLETCHER INCORPORATION, El Monte, California Senior Stress Engineer 7/98 - 2/99

Air load, stress, and fatigue analyses of F-18, and F-22 aircraft fuel, avionic pods. NORTHROP GRUMMAN CORPORATION, El Segundo, California Senior Mechanical Engineer of Kistler Program 2/98 - 6/98 Stress analysis of Orbital Vehicle upper stage composite structures (Umbilical Doors, Startracker, Airbag, and Parachute Deployment Mechanisms). THE BOEING COMPANY, Long Beach, California

Senior Mechanical Engineer of C-17 Program 9/86 - 2/98 Stress analysis and evaluation of composite material design and performance EDUCATION

Master of Science - Mechanical Engineering - California State University, Long Beach Concentration: Composite Material Design and Analysis Thesis: Design and Analysis of An Automatically Controlled Impact Sensing Mechanism With Aerothermoelasticity and Aeroservoelasticity

Bachelor of Science - Mechanical Engineering - San Jose State University, San Jose Concentration: Dynamics and Stress Analysis

CERTIFICATES OF ACHIEVEMENT

Northrop Grumman Corporation (NGC), El Segundo, California NCASA

SLIM Vision

CATIA V5 Navigation

IDAT (Integrated Detail Analysis Tools)

IMAT (Integrated Metallic Durability and Damage Tolerance Analysis Tool) Goodrich Aerostructures Group, Chula Vista, California MSC NASTRAN/PATRAN 2005a

ENOVIA LCA V5 (data base)

CATIA V5

The MacNeal-Schwendler Corporation (MSC Institute of Technology), Costa Mesa, California NASTRAN 69

PATRAN 6.2-BETA

McDonnell Douglas Aerospace, Long Beach, California Pro/MECHANICA17

UNIGRAPHICS Versions 9, 10, 11, and 13

ANSI Y14.5M-1982 Dimensioning and Tolerancing for Engineers

Contact this candidate