Engineer Data

ARTURO GREEN

**** *. ******* *** *** *** Telephone: 818-***-****

Glendale, CA 91202 E-Mail: ************@*******.***

EXPERIENCE SUMMARY

Several years of experience in estimating aircraft component loads as a

design loads engineer

Estimation of hydrostatic loads and generation of structural proof test pad

loads for static test

Experienced in tracking and correlating measured flight test data as

structural flight test engineer

Supported structural flight testing of military and civilian aircrafts for

safety of flight and certification

Process development and enhancement using proprietary software such as

Excel and Fortran

PROFESSIONAL EXPERIENCE

Belcan TechServices, East Hartford, CT 3/13-Present

Contract Ground Test Engineer (Aircraft component testing)

Developed Excel Macro to process test data

Reviewed supplier test plans, results and FAIs for system compliance

Derived forcing frequencies for vibration endurance testing to qualify

pilot/co-pilot seat

Project: Sikorsky CH-53K

CTS International, Bellevue, WA 11/10-8/11

Contract Loads Engineer (Aircraft component loads computation)

FORTRAN code re-hosting to UNIX platform

Loads validation

Wind tunnel data reduction using Excel and detail weight distribution on

FEM

Project: Boeing KC-46 Tanker

Northrop Grumman Corp, El Segundo, CA 10/04-4/10

Level 4 Loads Engineer (Aircraft component loads computation)

Development of balanced component loads and distributing results on

internal loads FEM

Developed optimization technique to simultaneously compute weights for

several non-symmetric fuel tanks to achieve target weight and cg

Developed method to derive optimum pad loads for static test

Developed method to reduced time to develop balanced loads by over 30

percent and automated loads process resulting in eliminating the

possibility of introducing errors and reducing overall loads development

time.

Arturo Green Page Two

Estimated hydrostatic loads for fuel tanks

Selection of critical design cases and extraction of inertia and air load

distribution for structural ground test

Created OML surface pressure database and Excel macro to extract and

annotate max and min surface pressures on grid points for panel design

Checked BDFs for errors and made corrections using in-house code and PATRAN

Provided localized pressure data for seal design

Project: JUCAS, F-18

4/02-9/04

THE BOEING COMPANY, Houston, TX

Level 4 Loads Engineer (Space Transportation System component loads

computation)

Computed Space Shuttle solid rocket engine nozzle on launch pad deflections

associated with wind forcing function to determine required clearance

between platform and propulsion element and presented results to NASA loads

panel

Predicted Space Shuttle critical component loads at high Q due to winds

aloft on day of launch in support of launch commit criteria

Conducted debris transport analysis in support of the STS-107 accident

investigation

Evaluated and certified SRB assembly for flight and reduced post flight

Ignition Over Pressure data

Project: Space Transportation System (Space Shuttle)

RAYTHEON AIRCRAFT COMPANY, Wichita, Kansas 1998-2001

Lead/Sr. Loads Engineer (Aircraft component and store loads computation)

Lead engineer for defining preliminary loads on model 450

Responsible for computing component design loads per CFR Part 23 for the

Joint Primary Aircraft Training System (JPATS) using 6DOF simulation

Development of software using FORTRAN to compute store cg loads for JPATS.

Developed method to distribute net loads on an external fuel tank for

selected conditions using Microsoft Excel

Supported loads flight-testing of JPATS by monitoring real time measured

loads, and extrapolated data for envelope expansion.

Computed maneuver, static gust, landing and ground handling component loads

for JPATS

Authored the flight test report to certify JAPTS for use by the USAF and

USN

Computed continuous PSD gust loads using NASTRAN results to update CFR Part

25 loads

Projects: T-6A (JPATS), Beechjet Model 400A, Model 450

Arturo Green Page Three

CESSNA AIRCRAFT, Wichita, Kansas 1995-1998

Loads Engineer (Aircraft component loads computation)

Developed software to correct wing side of body CP data, corrected vortex

lattice calculations

using wind tunnel data to accurately estimate wing air load distribution to

generate CFR Part 25 design loads.

Computed disconnect elevator loads per CFR Part 25

Estimated wing, flaps and control surface loads

Computed maneuver, landing and ground handling component loads

Projects: Cessna Citation 560 Excel

Temporary non-technical employment (1990-1994)

MCDONNEL DOUGLAS, St. Louis, Missouri 1988-1990

Sr. Loads Engineer (Store loads analysis and measurement for captive

carriage)

Responsible for computing store hardware interface and cg loads,

investigation of store

impact on overall wing loads, flight parameter modifications to obtain

desired loads results

interface with stress to expand interface hardware strength envelope, and

supported flight

test efforts for store captive carriage qualifications.

Projects: F/A-18, T45

GRUMMAN AEROSPACE CORPORATION, Bethpage, NY 1983-1988

Structural Flight Test Engineer (Measurement of aircraft component loads

with strain gages)

Planned ground test, interfacing with instrumentation engineers to maintain

data quality and to evaluate strain gage health, real time monitoring of

flight loads for safety of flight, data tracking for envelope expansion and

analysis of test data.

Lead engineer for evaluating the impact of ECS exhaust on composite

structure

Effective time-roll constant calculation for flying qualities evaluation

Recorded Cooper Harper rating assessment from pilot in the loop simulation

sessions

Projects: X-29 (Edwards AFB), A-6F

The Boeing Co., Seattle, WA 1980-1982

Structural Flight Test Engineer (Measurement of aircraft component loads

with strain gages)

Developed software to compute theoretical moment and torsion arm for

calibration

Created test plans for to measure horizontal tail center section loads

Interfaced with instrumentation engineers to maintain data quality

Arturo Green Page Four

Real time monitoring of flight loads for safety of flight

Reduced and transmitted measured loads to design engineers

Filtered and reduced accelerometer data

Generated PSD data for design engineers

Projects: 767-200

EDUCATION

Polytechnic Institute of New York, Brooklyn, NY

Bachelor of Science, Aerospace Engineering, 1979

TRAINING AND OPERATING SYSTEMS

Finite Element Analysis

Unsteady Aerodynamics

Jet Transport Performance Method

ZONAIR

PATRAN

NASTRAN

AUTOCAD

CATIA V5

FORTRAN

C Program

VAX/VMS

IBM TSO

UNIX

Microsoft Word

Microsoft Excel

Microsoft Access

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