Arman Motamedi Nazari

Arman Motamedi Nazari Email and Phone Number

Owner, President at Global Technical Resources - GTR | Aerospace Engineering | Senior Structural Stress, L&D Engineer, Methods | Technical Advisor | Defense Consultant | @ Global Technical Resources - GTR
Arman Motamedi Nazari's Location
Anaheim, California, United States, United States
About Arman Motamedi Nazari

I am a seasoned aerospace engineer with over 25 years of experience specializing in stress analysis, FEM modeling, and structural substantiation for aircraft systems. As the Chief Engineer at Global Technical Resources, I lead cutting-edge projects in STC structures, external pod installations, and innovative conceptual developments for drones and eVTOL systems. My career spans work with industry leaders such as Boeing, Bombardier, and Virgin Galactic, where I have contributed to advanced aircraft programs and mission-critical projects.With expertise in hand calculations, FAA compliance, and cutting-edge software like PATRAN, FEMAP and NASTRAN, I thrive in delivering innovative, safe, and efficient solutions for the aerospace industry. My portfolio includes commercial and military aircraft, UAVs, and business jets, demonstrating my versatility and passion for advancing aerospace technology.Beyond engineering, I am deeply committed to fostering professional growth within the aerospace community and sharing insights to drive innovation. Let’s connect to explore how we can shape the future of aerospace together.Cell/Text 626.755.8989anazari@globaltechres.com

Arman Motamedi Nazari's Current Company Details
Global Technical Resources - GTR

Global Technical Resources - Gtr

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Owner, President at Global Technical Resources - GTR | Aerospace Engineering | Senior Structural Stress, L&D Engineer, Methods | Technical Advisor | Defense Consultant |
Arman Motamedi Nazari Work Experience Details
  • Global Technical Resources - Gtr
    President, Chief Engineer
    Global Technical Resources - Gtr Oct 2023 - Present
    In my role as President and Chief Engineer at Global Technical Resources - GTR in Anaheim, California, I provided crucial support for structural stress analysis, certification reports, maintenance manuals and repair approval, created automatic tools for calculation using Excel and VBA, supported test articles and test coupons, and produced fatigue, DT/DTA and reliability analysis based on design service life. Weight and Balance analysis. Prepared finite element models. Performed hand calculation of components based on clients manuals. Generated Load & Dynamics reports for air vehicles. Wrote and programmed formula for methods.
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  • Boeing
    Service Engineer (Se)
    Boeing May 2023 - Sep 2023
    Arlington, Va, Us
    Service Engineering (SE), supporting Boeing fleet globally. Boeing Operation Center Integrated Team provides support to customers Service Requests (SR) for Aircraft on Ground (AOG). I worked with the Rapid Response Team providing permanent, temporary and time- Limited repairs & evaluations based on Priors, Structural Repair Manual (SRM) and Aircraft Maintenance Manual (AMM) within a two-hour window. Used Boeing Communication Systems (BCS), REDARS, ACT, Illustrated Parts Catalogue (IPC), Master Minimum List of Equipment of all types of Boeing aircraft Models. Followed FAA guidelines for repair and Continued Airworthiness Safety Program (COSP) evaluation. Other tasks included archiving,writing backlog reports for repairs and coordinating with CASTLE. Used Boeing tools such as My Boeing Fleet, Salesforce. Attended various courses from Customer Support and Communication to Export Control as required.
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  • Aurora Flight Sciences
    Senior Stress Analyst
    Aurora Flight Sciences May 2022 - Mar 2023
    Manassas, Va, Us
    Aurora Flight Sciences is a Boeing company. I performed Structural Analysis for Twin Fuselage Airplane. Structural joints interface loads and sizing of the fittings. Joints included engines, fuselage, and launch pylon interface to the wing. Stress analysis, finite element Modeling, design and production support.
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  • Virgin Galactic
    Senior Stress Analyst
    Virgin Galactic Jul 2019 - Jan 2021
    Tustin, Ca, Us
    Working on White Knight 2 (WK-2) wing structure. This is the launch plane for the Spaceship II with double fuselage. Structures include Skins, Ribs, Spars, and Shear webs. All parts are composites as well as joints. Responsibilities includes checking structural integrity of bondline joints and parts for static strength and stability. Structural Damage tolerance assessment, MRB, modifications, mitigations and design evaluations.
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  • Gtr Global Technical Resources
    Senior Stress Analyst | Consultant
    Gtr Global Technical Resources Jan 2019 - Jun 2019
    Installation of Ampaire Electric Motor on Cessna 337 Skymaster. The conversion program involved replacing one of the aircraft’s two piston engine with an electric-propulsion system. On 22 November, the company flew the modified aircraft,which it calls the Electric EEL, round trip from Kahului to Hana, both on Maui. Installation of electric motor, inverters, high powered electronics, and related systems. Ampaire and services provider Ikhana Aircraft Services conducted a study for the feasibility of equipping de Havilland Canada DHC-6 Twin Otters eVTOL with hybrid electric propulsion.Familiar with FAR Part 21.17 (b) Type certification of very light airplanes, EASA SC-VTOL-01 European Union Special Condition for Small Category Vertical Take Off and Landing (VTOL) aircraft Type Certificate and (eVTOL), and JARUS CS-LUCAS.
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  • Ikhana Group, Inc
    Senior Stress Analyst
    Ikhana Group, Inc Jul 2017 - Jan 2019
    Finite element modeling using Femap and classical hand calculations are used to provide support for repair, MRB, modifications, and sizing substantiation for special mission aircrafts. Interfacing with FAA DERs for approval of stress reports, and PSCP (project specific certification plan) reviews. Modifications include addition of antennas, pods, and radome for special mission aircraft. Increase of MTOW, reengining of aircraft, and modification of interior for VIP in support of various STCs. Reengining of Twin Otter from Pratt and Whitney to General Electric. Installation of Radar Laser on special mission aircraft.
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  • Mooney International Corporation
    Senior Stress Analyst
    Mooney International Corporation Jan 2017 - Jul 2017
    Kerrville, Texas, Us
    Stress Engineer, TestingPreparing development test plans for Mooney new all composite aircraft spar skin wing box. The activity included developing new spread sheets for calculations, constructing FEM of the test specimen and the support fixture. Substantiate the strength and stability of the specimen and fixture. Establish failure criteria for the test. Correlate the FEM and hand analysis results. Witness testing. Test plans included bondline strength for shear clips, Spar Strength, Spar global buckling, ramp and impact testing.
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  • Utc Aerospace Systems
    Senior Stress Analyst
    Utc Aerospace Systems Jan 2016 - Jan 2017
    Charlotte, Nc, Us
    Subject Matter ExpertJoined exciting environment of production MRB of composite structures. Providing repairs for components of Thrust Reversers. Checking reports from ODC (Offshore Design Center) to ensure the correctness and compliance with the company methods as well as governing rules and requirements. Coordinating activities with ODC, manufacturing, quality and liaison engineering by holding multiple daily meeting. Providing innovative methods to decrease MRB tag, process time. Coordinating activities with, and providing solutions to European and Asian supplier. Interfacing with Airbus to update and implement new methods of calculations. Helping new teammates to get familiar with company methods. Providing quick studies to MRB QNs in order to better classify the repairs for engineering teams. Writing VBA Codes, using SAP & Teamcenter.
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  • Ressources Techniques Globales
    Senior Stress Analyst
    Ressources Techniques Globales 2010 - Jan 2017
    Founded Ressources Techniques Globales in 2010. The Company is a Canadian, Quebec Corporation Located in Montreal, Quebec, Canada. The company provides Technical Talent, Consulting Services and Material Supplies to Global Industry.
  • Gulfstream Aerospace
    Senior Stress Analyst
    Gulfstream Aerospace Aug 2012 - Nov 2015
    Savannah, Ga, Us
    Stress Engineer; AAP (Advance Aircraft Program)Joined the wing group and immediately started working on the following structures; MLG Uplock Fitting, Ribs, Forward Spar, Fuel System Instl’n, Skin Stringer, Stringer Run Out, Splice Stringer, Fix Leading Edge, Fix Trailing Edge. Used Nastran and Patran for Modeling and development of internal loads, Pyloads and loadrep for load extraction and formulation, Catia V5 & Smarteam for drawing retrieval. Creating FEM of IB/MID/Fix Trailing Edges using MSC Patran/Nastran. Writing Certification Report for FAA.
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  • Northrop Grumman Corporation
    Senior Stress Analyst & Mrb Engineering Consultant
    Northrop Grumman Corporation Feb 2012 - Jun 2012
    Falls Church, Va, Us
    BAMS UAV
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  • Bombardier Aerospace
    Senior Stress Analysis Consultant
    Bombardier Aerospace Jun 2010 - Feb 2012
    Dorval, Québec, Oo
    Cseries, Cockpit, NLG Box Sizing.Cockpit System Installation, Forward Fuselage, Door Surround.
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  • Spirit Aerosystems
    Senior Stress Analysis & Mrb Engineering Consultant
    Spirit Aerosystems Feb 2009 - Aug 2009
    3801 S Oliver St, Wichita, Ks, Us
    Stress Analysis of Metallic & Composite Structures as well as Supporting Rejection Tags and MRB. Primary and Secondary Structures. Fix Leading and Trailing Edge, Ribs, Spars & Skins. Hand Calcs & FEM. EXCEL, Nastran, PATRAN & CATIA V5.A/C G650.
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  • Nordam Tulsa
    Senior Stress Analysis Consultant
    Nordam Tulsa Feb 2006 - Feb 2009
    Tulsa, Ok, Us
    Stress Analysis of Metallic & Composite Structure as well as Supporting Rejection Tags and MRB. Worked on Engine Cowl Door, Hinges, Fan Duct,Thrust Reverser, Nozzle, EBU, Fan Cowl, Inlet Cowl & BLKHD. Hot and Cold Temperature.Hand Calcs & FEM. EXCEL, Nastran, PATRAN & CATIA V5. A/C Falcon 2000EX, G450 and Hawker Horizon, Cessna, Gulfstream & Learjet.
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  • Boeing Commercial Airplanes Long Beach
    Senior Stress Analysis Consultant, Loads & Strength Group
    Boeing Commercial Airplanes Long Beach May 2005 - Jan 2006
    Arlington, Va, Us
    Stress Analysis, Static, Fatigue & DT/DTA Boeing Method.StaticPrimary Metallic Structure, Detail Stress Analysis, 747-LCF (Large Cargo Freighter). Fatigue The Frames webs and caps were reinforced by doublers and straps and a detail Ultimate & Fatigue (Book 1 & 2) stress analysis was performed using SA, IAS, JOLT, IDTAS,FEADMS & VISIO. Detail Fatigue Rating (DFR) of Fittings. Frame Stabilization and penetration holes, sizing and strength were also part of report.DT/DTA767 SRM (structural repair manual ) Residual Strength & Damage Tolerance. Book 3 & 4 methods are used in conjunction with JOLT, DTANAL MAGIC Residual Strength and Crack Growth. Threshold analysis and Inspection. 777 Interior FEM using Nastran/PATRAN. FEM of various interior options such as galleys and ceilings.
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  • Goodrich Aerostructures
    Stress Analysis Consultant
    Goodrich Aerostructures Jun 2004 - May 2005
    Stress Analysis of Metallic Structure, as well as Load generation. Hand Calcs & FEM. Primary Structure. Engine Pylon. EXCEL, Nastran/Patran & Catia. A/C C5 Galaxy.
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  • Sargent Fletcher El Monte
    Stress Analysis Consultant
    Sargent Fletcher El Monte Jan 2004 - Jun 2004
    Detail Stress Analysis of External Fuel Tanks and Pods, ATA Refueling Pneumatic Release Equipment, Aircraft Special Purpose Pods. Hand Calcs & FEM. EXCEL Nastran/PATRAN.A/C KC130 and etc.
  • D3 Technologies - The Leader In Autodesk Manufacturing Solutions
    Stress Analysis Consultant
    D3 Technologies - The Leader In Autodesk Manufacturing Solutions Sep 2003 - Oct 2003
    Springfield, Mo, Us
    Stress Analysis of Primary Metallic Structure, Stringer Runout Calculation for APB Winglet addition. Stringer Reinforcement. JOLT was used for 737 BGW to generate loads at the fasteners. Durability (Book2) methodology was to be applied for Detail Fatigue Rating (DFR) by using IAS and IDTAS. Project got cancelled.
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  • Boeing
    Stress Analysis Consultant
    Boeing Oct 2000 - Sep 2002
    Arlington, Va, Us
    Stress Analysis of 737, 757 Mechanical Systems team. Supporting Laison, Design and Airlines repairs. These include Providing solutions to telexes and design requests on the day to day basis and writing and filing reports. IAS and Kball. Checking the control circuits for jamming and compliance to FAR , DR&O requirements and assurance of dual load paths. Wind milling requirements such as forced fatigue and vibration in conjunction with Electrical Installation Group on the electrical racks checking compliance with ERINC. March of 2001 at Everett Plant working on 777 with structure Payloads group. OSU, OFCR (Overhead Flight Crew Rest) 777 ER/LR. Composite Structure. Hand Calcs & FEM. EXCEL, Elfini, Nastran/PATRAN & IAS.
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  • Bombardier Aerospace, De Havilland Toronto
    Stress Analyst
    Bombardier Aerospace, De Havilland Toronto Jan 1995 - Oct 2000
    Dorval, Québec, Oo
    Stress Analysis of VSTAB and HSTAB of GLOBAL EXPRESS- business jet -certification reports, leading edge bird strike, rudder VSTAB interfaces (hinges) and panels (skin stringer ) analysis. DASH8 Series 100/200/300 sustaining team. DASH8 Q 400 internal and external structural OPTIONS such as antennas for GPS, mechanical systems such as Aft Entry Portable Folding Stairs, Cargo Door, Passenger Doors with Vent Door Mechanism. Installation of galleys, Carts , Trolleys and Inserts as well as Aft and Fwd Baggage Compartments and corresponding Bulkheads different configurations and writing reports Tabulating Margin of Safety (Global Express & Q400) & Reserve Factors (DASH8 S/100,200 & 300). Hand Calcs. A/C DASH-8 & Global Express.
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Arman Motamedi Nazari Education Details

  • Ryerson University
    Ryerson University
    Aerospace Engineering

Frequently Asked Questions about Arman Motamedi Nazari

What company does Arman Motamedi Nazari work for?

Arman Motamedi Nazari works for Global Technical Resources - Gtr

What is Arman Motamedi Nazari's role at the current company?

Arman Motamedi Nazari's current role is Owner, President at Global Technical Resources - GTR | Aerospace Engineering | Senior Structural Stress, L&D Engineer, Methods | Technical Advisor | Defense Consultant |.

What schools did Arman Motamedi Nazari attend?

Arman Motamedi Nazari attended Ryerson University.

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