OSAYANDE OMOND IAGBE

Home: ** ***** ***** *****, **** Park, MA 02136

acpn2y@r.postjobfree.com 617-***-****

WI L L I NG TO RELOCATE

SUM MARY

Highly focused, disciplined, int r insically motivated engineer, skilled in applying scientific

p rinciples in design, structure and stability analysis, testing, manufacturing and industrial

technology.

Assisted in standardization of geothermal and HVAC component lists for suppliers.

Strong analytical mind and effective use of initiative in engineering projects.

SKI L LS: SolidWorks, Mathcad, MAT LAB, Advanced Aircraft Analysis (AAA), COMSOL,

SAP, LabVIEW, M icrosoft Office and Mac applications (Word, Excel, PowerPoint, Visio, etc.).

EDUCAT ION

Daniel Webster College, Nashua, NH

Bachelor of Science; Aeronautical Engineering [ ABET Accredited] M inor: Business Management

GPA: 3.51 Graduated: May 10th 2014

COURSEWORK

Aircraft Design Aircraft Structure Flight Dynamics Aerodynamics Control Systems Engineering

Mechanics of Materials Material Science Propulsion D ifferential Equation T hermodynamics F luid

Mechanics Heat Transfer E ngineering Capstone

ENG INEER ING PROJECTS

SENIOR AIRCRAFT DESIGN PROJECT - D ESIGN AND FABRICATION OF AN AIRCRAFT

Project involved the design and fabrication of an 8lb. aircraft to take off, climb to

m inimum 100 feet above ground level, record and display altitude with the use of Data

Acquisition System (DAS), and laptop, then drop a humanitarian aid package onto a

t arget with use of a First Person View system (FPV), and land intact. A big part of the

p roject was designing a 15lb. static payload with boundaries that fit into the aircraft

w ithout adding any structure to the aircraft design. Also, a 3lb. payload (to simulate

t he humanitarian package) was designed which drops from the aircraft with the use of

t he DAS. The integration of both payloads into the aircraft without exceeding the

weight requirement was a success and the design was one of the best at 2014 SAE Aero

Design Competition.

MOTORIZED LONGBOARD

Project involved design and build of alternative means of t ransportation to incorporate a

longboard with two electric motors at rear wheels, a pulley and belt system, controlled by a

handheld wireless controller and powered by high capacity batteries.

EXPER IENCE

I NTERN Bosch Thermotechnology, Product Management Division, Londonderry, N H

November 2013- February 2014

Supervisor: Wade Reily, M anager of Spare Parts

Assisted in standardization of geothermal and HVAC component lists for suppliers

t hrough use of spreadsheets

Coordinated data collected to upload on company’s “Webshop”

Performed data entry and ret rieval using SAP

FACULTY ASSISTANT, Engineering Department Daniel Webster College, Nashua, NH

January 2013 – May 2014

Assisted Dean N. Bertozzi and Prof. M. Sadraey

Delivered tutoring sessions on Flight Dynamics and Electrical Engineering, as well as

w ind tunnel lab exercises

Provided exercises on wind tunnel calibration

M ACHINE SHOP ASSISTANT, Engineering Department Daniel Webster College, Nashua, NH

January 2014 – May 2014

Assisted Dean N. Bertozzi

Assisted student with projects in machine shop

Performed part creation with Bridgeport and CNC MA K INO M illing machine

Gained experienced with CAMWORKS for creating CNC tool path

Engineering TESTS (Test performed with Cessna 172R)

PITOT-STATIC ERROR CALIBRATION: To determine the t rue airspeed and calibrated

a irspeed of the aircraft, and find the static position error with respect to calibrated airspeed

POWER REQUIREMENTS: To determine the power available and required for level f light

and the maximum rate of climb for the aircraft

TURN PERFORMANCE: To determine the turn radius and rate of the aircraft

NEUTRAL POINT: To determine the neutral point of the aircraft

LATERAL-DIRECTIONAL STABIL ITY AND ROLL POWER: To determine if the C-172R meets

t he FAR 23 requirements for roll performance, and check the lateral-directional stability of the

a ircraft

DYNAMIC STABIL ITY: To quantify the longitudinal short period and Phugoid dynamic

s tability to characterize the spiral instabili ty and Dutch roll of the aircraft

ACT IV I T I ES

Alpha Chi; Member

American Institute of Aeronautics and Astronautics, AIAA; Member

Design Build Fly, DBF; Member

Sigma Gamma Tau; SGT; Member

2

Society of Automotive Engineers, SAE; Member

Awards

Sigma Gamma Tau Northeastern Regional Award winner – 2014

SAE Aero Design Competition, 3rd P lace Oral Presentation in Advanced Class – 2014

ASEE Zone 1 Student Posters Competition, Honorary Mention – 2014

SAE Aero Design Competition, 4Th P lace overall in Advanced Class – 2014

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