Rotorcraft Weights Engineer

About CFD Research: Since its inception in 1987, CFD Research has delivered innovative technology solutions within the Aerospace Defense, Biomedical Life Sciences, Intelligence Sensing, and Energy Materials industries. CFD Research has earned multiple national awards for successful application and commercialization of innovative component/system technology prototypes, multi-physics simulation software, multi-disciplinary analyses, and expert support services. Based in Huntsville, Alabama where laboratory facilities and headquarters are located, CFD Research also has office and laboratory facilities in Dayton, Ohio, prototyping test and evaluation facilities in Hollywood, Alabama, and office facilities in Fort Walton Beach, Florida.

CFD Research is an ISO9001:AS9100D registered company and is appraised at CMMI Level II for Services. CFD Research is a 100% ESOP (employee-owned company) recognized in Inc. Magazine's Inc5000 as a top growing company for four of the last five years.

S. Army Aviation Missile Center’s (AvMC) Technology Development Directorate (TDD). The engineer will apply existing computational tools, develop new computational methods, and build models in specialized areas such as cost, propulsion, and parametric design to support rotorcraft conceptual, preliminary, and detailed component design activities.

This position will support the Conceptual Design and Assessment (CD A) branch with a focus on developing aircraft weight trends, formulation and update of weight equations, and conducting detailed weight assessment of aircraft. The position will assess air vehicle performance and weights and support the team’s assessment of cost and operational capability.

Requirements

, assess ongoing aircraft development programs, and provide technical expertise to TDD for future air vehicle concepts and exploratory design initiatives.

trade space and provide guidance on operational impacts of design features as they relate to operational

Assess current technologies and collaborate with other technical disciplines to provide system-level assessments of component technologies. Collaborate with a team to develop and test new tools used in the design process.

Responsibilities

: Collect and curate data necessary to formulate updates to weight equations, develop weight trends, and apply these trends to aircraft studies as needed. Perform detailed assessment of vendor aircraft and compare component weights to existing trends. Utilize government-standard tools, such as NASA Design and Analysis of Rotorcraft (NDARC), for detailed aircraft modeling and performance assessment.

Provide expert input on technology factors used in calibration of NDARC models.

Required Qualifications

: 10+ years of experience performing conceptual design of rotorcraft manned/unmanned systems, estimating aircraft performance and weights. S. in Aerospace Engineering, Mechanical Engineering, or related field from an accredited college or university.

Direct experience performing weights analyses and developing component and system level weight trends. Experience developing aircraft designs and estimating performance using NDARC and Air Vehicle Integrated Design Environment (AIDEN). Experience conducting aircraft trade studies to define and explore trade space.

S. Citizen. Ability to obtain and maintain a DoD Secret security clearance.

Preferred Qualifications

S. in Aerospace Engineering, Mechanical Engineering, or related field from an accredited college or university. Advanced knowledge of rotor conceptual design process.

Demonstrated ability to work independently and lead technical efforts with minimal oversight.