Satya Ghoman, Ph.D. Email & Phone Number

Washington, Dc, Us

Washington D.C. Metro Area

Leadership Responsibilities: Plan, lead and manage multiple commercial projects in capacity of Project Manager and Technical Project Lead. Member of the Project Management Office (PMO). Conduct multi-functional team integration. Define scope of work based on contractual requirements. Ensure on-schedule and within-budget project performance. Serve as the primary contact person and/or subject matter expert for technical monitors of commercial clients. Provide mentoring for new staff and interns.Technical Responsibilities: Deliver advanced analysis-driven solutions for challenging engineering problems. Lead multiple commercial contract activities and provide technical expertise on a wide range of structural dynamics analyses, static and dynamic aeroelasticity, and detailed stress analysis of aerospace structures.

Scottsdale, Arizona

Technical Responsibilities: R&D Specialist for structures, aeroelasticity, flight loads, aircraft design, and multi-disciplinary optimization. Provide technical expertise to federally funded research contract activities. Actively respond to NASA and DoD solicitations by proposing innovative research. Make substantial personal technical contributions to IRAD (Independent Research and Development) activities. Lead/Assist in engineering software product development/integration/testing. Provide technical consultation and training for government/commercial clients.Leadership Responsibilities: Plan, lead and manage federally funded projects in capacity of Principal Investigator and/or Technical Project Lead. Serve as the primary contact person for federal contract technical monitors, and subcontractors.

Blacksburg, Virginia

Study of multi-disciplinary structural shape and sizing optimization of a concept Supersonic Transport aircraft wing. Aimed at weight minimization and aeroelastic performance enhancements.Developed an innovative Reduced Order Modeling (ROM) scheme for a multi-fidelity MDAO framework for shape and sizing optimization. Designed a supersonic transport aircraft concept for aerodynamic and structural loads under various performance conditions.

Scottsdale, Arizona

Developed a Multi-disciplinary, Multi-fidelity and Multi-strategy (M3) Design and Optimization framework. Developed and implemented parallel HPC, smart job assignment, and effective resource management.Developed modules for results database generation, data mining and post-processing.Performed the Shape and Sizing optimization of the wing of a Generic Business Jet (based on Gulfstream G500).Documented and presented the framework and results for submission to NASA.

Norfolk, Virginia

Worked for a NASA-funded research contract: Developed a FEM-based solver to analyze nonlinear flutter of curved panels of aircraft under yawed supersonic flow at elevated temperatures.

Phd, Aerospace Engineering

Dissertation: A Hybrid Optimization Framework with POD-based Order Reduction and Design-Space Evolution Scheme Selected Courses.

M.S., Aerospace Engineering

Thesis: Nonlinear Flutter Analysis of Curved Panels under Yawed Supersonic Flow and at Elevated Temperatures Using Finite Elements