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 Air Vehicle Optimization Group at UDRI is a diverse team of skilled engineers and scientists who work closely with the Air Force Research Laboratory (AFRL) to develop, prototype, and test numerical models, software, and hardware for the multidisciplinary design and analysis of aerospace vehicles. The group brings together specialties in Aerospace, Electrical, and Mechanical Engineering, Computer Science, Mathematics, and Physics to combine state-of-the-art engineering tools with innovative ideas to support future aircraft design methods from conceptual design through flight testing. A few of the projects the group currently supports include: Computational Aircraft Prototype Synthesis (CAPS), Missile Enhancement via Reconfigurable Interceptor Nose, Efficient Supersonic Aircraft Vehicle, X-56, XQ-58, Effectiveness Assessment of Concepts and Technologies, and Sensitivity Analysis for Multidisciplinary Systems.
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
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.
Closing Statement:
Informed by its Catholic and Marianist mission, the University is committed to the dignity of every human being. Informed by this commitment, we seek to increase diversity in all of its forms, achieve fair outcomes, and model inclusion across our campus community. The University is committed to policies of affirmative action designed to increase the employment opportunities of individuals with disabilities and protected veterans in compliance with the Rehabilitation Act of 1973 and Vietnam Era Veterans' Readjustment Assistance Act of 1973.
Whatsapp Facebook LinkedIn Email App
Employers have access to artificial intelligence language tools (“AI”) that help generate and enhance job descriptions and AI may have been used to create this description. The position description has been reviewed for accuracy and Dice believes it to correctly reflect the job opportunity.
- Dice Id: RTX162c2a
- Position Id: 132d3ac517ecb22883c479ee878ca13e
- Posted 1 day ago
Never miss an opportunity! Create an alert based on the job you applied for.
