Engineer Design

VLADIMIR ALEKSOV

*** *** *** *, **** #** Phone: 206-***-****

Kirkland, WA 98033, USA Home E-mail: ac5gnq@r.postjobfree.com

CORE PROFESSIONAL SKILS:

Aircraft load estimation: flight load evaluation for various types of maneuvers, gust and rundom turbulence loads, control surface deflection load, flight loads survey.

Aerodynamic: aerodynamic force and moment coefficient estimation, wind tunnel, CFD and flight test, aerodynamic database for simulation development, flight mechanics and performance calculation.

Aircraft stability and control: stability analysis, handling qualities, flight dynamic, control system design, ground, flight test and certification.

Structural Analysis: structural static, fatigue and damage tolerance analysis of aircraft primary and secondary metallic and advanced composite structure.

Simulation: mathematical models of the aircraft aerodynamics and system development, flight simulation.

Regulation: design requirement formulated in accordance with EASA, CFR23, CFR25 and MIL standards, certification procedure, design and preparation of technical documentation for Certification.

CAREER HISTORY:

2016-present Loads and Dynamics Engineer – Mitshubishi Aircraft Company – Nagoya – Japan

Loads and aeroelastic stability evaluation for interaction of systems and structures for MRJ 200. Supported flight test (flight loads survey). Wrote certification documents.

2013-2016 Senior Aerospace Loads Engineer – TLG Aerospace – Seattle – USA

On various aircraft models (Boeing 737, 757 and 767) perform aircraft static aeroelastic loads analysis supported by CFD, wind tunnel pressure model and flight testing. Prepare aerodynamic data bases for use in external loads and dynamics. Analysis of external aircraft static loads for flight, ground and landing impact. Perform aircraft external dynamic loads analysis considering the random nature of atmospheric turbulence and the effect of automatic flight control systems in determining structural responses and loads distributions.Wrote certification documents.

2004-2012 Loads and Dynamics Engineer – Boeing - Seattle – USA

Structural design loads and fatigue analysis of wing control surfaces and High-Lift (flaps, slats, leading edge, Krueger flap, trailing edge and flap support fairings) for Boeing 787-8-9-10, Boeing 747-8, Boeing 767-K46 and Boeing 777-EW-9x. Supported flight test (flight loads survey) for the Boeing 787-8. Wrote certification documents.

2002-2004 Loads and Dynamics Engineer – Aviation Partners Boeing – Seattle - USA

Structural design and fatigue loads analysis of wing, winglet (blended winglet technology) and the other components (fuselage, engine, empennage and etc.) for Boeing 737-300, Boeing 737-400, Boeing 767-300 and Boeing 757-200 with APB winglet retrofit kit. Supported flight test (flight loads survey) for the Boeing 737-300. Wrote certification documents.

1999-2002 Loads and Aeroelasticity Engineer – Embraer - Brazil

Analyzed dynamic response and calculated loads of vertical and lateral gust (continuous turbulence) for EMB 145SA aircraft. Performed convergence study in the dynamic response of continuous turbulence and defined cut off frequencies for ERJ 170 aircrafts. Stability and handling qualities assessment due to dynamic gust response. Wrote certification documents.

VLADIMIR ALEKSOV

1998-1999 Loads and Dynamics Engineer - Fairchild Aerospace – Dornier - Germany

Wing control surface (aileron) aerodynamic loads, with aerodynamic database participation for simulation development (728 Jet ).Structural Analysis for CF-34-8D engine, nacelle and pylon (728 Jet). Structural Analysis for APU and support structure (728 Jet).

1996-1998 Loads Engineer – IPTN - Indonesia

Performed fuselage static loads analyses on N250 turboprop aircraft. Loads in low speed maneuvers on N250. Calculated preliminary sizing limit loads for the primary structure of the N250-200 (configuration of 28400 kg MTOW ). Conduct tests and evaluate Time Response Program for AirCraft Loads ( A six degree of freedom maneuver simulation program dedicated to the generation of design flight load conditions for aircraft structural analysis ).

1994-1996 Aerodynamic Loads Analysts (Methods Development) Exco Engineering - Canada

Assisted in developing computer programs for generation of net load distributions and finite-element nodal loads for structural analysis of static flight and ground conditions. Developed a computer program for the calculation of static aeroelastic forces on lifting surfaces (Vortex Lattice), and computer program for the calculation of unsteady aerodynamic influence coefficients by the Doublet-Lattice Method.

1992-1994 System Performance Engineer Menasco Aerospace - Canada

Performed dynamic analysis of integrated landing gear and flight control systems. Developed software to evaluate flight test data and upgraded dynamics programs and models as required. Prepared necessary reports and ensured landing gear design loads and analysis of dynamic performance meet customer requirements.

1989-1991 Loads and Dynamics (Methods Development) Engineer De Havillend - Canada

Time-history analysis of symmetric landing events on a level runway Flight load evaluation for various types of maneuvers, gust and random turbulence loads, control surface deflection load.

1980-1988 Lead Engineer for Flight Test Investigation Aircraft Co. UTVA - Yugoslavia

Project UTVA 75. Flight test investigation Calculated vibration levels on aircraft due to propeller unbalance (UTVA 75). Project LASTA. Lead flight test investigation from first flight to certification. Applied and implemented requirements of FAR 23/MIL specifications. Wrote certification documents.

EDUCATION:

M.Sc.; Aerospace Engineering; University of Belgrade, YU.

COMPUTER SKILLS:

Unix, Catia, Nastran, Patran, HyperWorks, Abaqus, NASGRO, Fortran, MATLAB and Simulink. Various print and graphic application inclding awide variety of Microsoft products.

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