Research Aerospace Engineer

Job No: 503787
Work Type: Staff Full Time (1500 hours or greater)
Location: Dayton, OH
Category: Research Institute Staff
Department: Air Vehicle Optimization - 250571
Pay Grade: R1/R2 - Exempt
Advertised: August 07, 2026
Applications close: August 21, 2026

Position Summary:
UDRI is seeking qualified applicants to apply for a Research Aerospace Engineer position. This position will work for the Air Vehicle Optimization Group of the Structures & Materials Division and is a full-time benefit eligible position that offers health, dental and vision insurance, retirement, disability, tuition assistance, vacation/sick accrual and holiday pay.

The group is currently seeing an Aerospace Engineer to support ongoing research and development contracts at Wright-Patterson Air Force Base in the Air Force Research Laboratory to provide support for airframe propulsion and power systems integration. Research Aerospace Engineers apply fundamental engineering principles to design, develop, document, maintain, and deploy software infrastructure and engineering analyses in the support of aerospace engineering research. Specifically providing support in the area of conceptual vehicle design in support of our Modular/Scalable UAS portfolio and perform finite-element-based structural sizing processes.

The successful candidate will bring to bear their skills and experience with one or more of the following: experience in aircraft design and propulsion and power system integration, finite element analysis for structural analysis, CFD for aerospace analysis, multidisciplinary analysis, sensitivity analysis, design optimization, aeroservoelastic design optimization, and aircraft trajectory optimization framework, and computer programming. Strong communication and interpersonal skills are essential and highly valued in this role.

Minimum Qualifications:
- A Bachelors or equivalent degree in Aerospace Engineering, Mechanical Engineering or related discipline from ABET accredited institution
- Knowledge of: propulsion systems, aeroelasticity, experimental aerodynamics, numerical analysis, CFD, orbital dynamics
- Basic experience with MATLAB, LabVIEW, Python, SolidWorks, OpenVSP, XFOIL, Cradle CFD, C++/Ansys or other similar programming languages
- Experience with developing 3D printed parts
- Due to requirements of our research contracts with the U.S. federal government, candidates for this position must be a US Citizen

R1 Level Requirements:
Bachelors and no previous work experience
R2 Level Requirements:
Bachelors and three years previous work experience, OR
Masters and two years previous work experience

Preferred Qualifications:
While not everyone may possess all of the preferred qualifications, the ideal candidate will bring many of the following:

- A Masters or equivalent degree in Mechanical Engineering, Aerospace Engineering, or related discipline from ABET accredited institution
- Proficient using MATLAB, LabVIEW, Python, SolidWorks, OpenVSP, XFOIL, Cradle CFD, C++/Ansys or similar programming languages
- Experience in designing and executing test procedures for parametric studies
- Experience with analyzing experimental data and presenting results
- Experience with mechanical design, experimental testing and validation, fluid mechanics, structural analysis, additive manufacturing, systems integration
- Experience with CFD tools
- Experience with designing and modifying propulsion test hardware
- Research experience

Special Instructions to Applicants:
To apply please submit a cover letter addressing each minimum qualification and any applicable preferred qualifications that you meet.

Whatsapp Facebook LinkedIn Email App