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Bob Stirling is a seasoned professional with extensive experience in the aerospace industry. He holds a Doctor of Philosophy (PhD) in Aerospace Engineering from the University of Bristol and a Bachelor of Science (BSc) in Aircraft Engineering from the University of Salford. Stirling has worked for various prominent companies, including British Aerospace, BAE Systems, and The Boeing Company, where he has held senior positions in flight control systems, aerodynamics, and stability and control. He has also founded and directed his own companies, including SDI Engineering and Stirling Dynamics. Stirling is proficient in multiple languages, including English, and has a strong background in systems engineering, finite element analysis, and program management. He has also developed expertise in avionics, military systems, and aircraft design.

Experience

  • STL Tech
    • Bristol, United Kingdom
    • Director
      • Jan 2019 - Present
      • Bristol, United Kingdom
    • Founder and Director
      • 1995 - Present
      • Seattle
  • Stirling Dynamics
    • Bristol, United Kingdom
    • Founder and President
      • Jan 1987 - Apr 2018
      • Bristol, United Kingdom
    • Lecturer & Research Fellow
      • Jul 1981 - 1990
      • Bristol, United Kingdom

      Flight mechanics and control, aeroelasticity, aeroservoelasticity. Primary flight control actuation systems. Carried out various MoD research contracts in collaboration with BAE Systems, Military Aircraft Division, Warton.

    • Control Systems Engineer
      • Jan 1981 - 1984
      • Portsmouth, United Kingdom

      Modeling, simulation and performance evaluation. Heavy weight torpedo control system and actuation. Continued after 1981 as consultant while at the University of Bristol.

  • British Aerospace, Military Aircraft Division, ...
    • Warton, Lancashire, United Kingdom
    • Principal Engineer, Flight Control Systems Department
      • Sep 1977 - Dec 1980
      • Warton, Lancashire, United Kingdom

      Modeling, simulation, analysis and design. Flight control systems, actuation systems and FCS/structural mode interaction. Tornado and Jaguar FBW (digital FBW research aircraft).

    • Senior Engineer, Dynamics Department
      • Jan 1974 - Sep 1977
      • Bristol, United Kingdom

      Aeroelasticity, flutter, gust loads, actuators. Active control systems research (gust load alleviation).

    • PhD Research
      • 1971 - 1974
      • Bristol, United Kingdom

      Active control technology research. Gust load alleviation and ride quality improvement for a commercial transport aircraft.

  • The Boeing Company
    • Seattle, U.S.A.
    • Aerodynamics Engineer, Stability and Control Department
      • 1965 - 1971
      • Seattle, U.S.A.

      747 and SST stability and control and stability augmentation system design.Modeling, simulation and analysis. Software methods and tools development.

    • Aerodynamics Engineer, Stability and Control
      • Apr 1964 - Nov 1965
      • Toronto, Canada

      DHC-6 Twin Otter stability and control and loads.Aerodynamic static and dynamic derivative estimation.

    • Aircraft Engineering Apprenticeship
      • 1957 - 1964
      • Manchester, United Kingdom

      Six year apprenticeship. After completing apprenticeship and BSc degree, employed as an Aerodynamics Engineer on aircraft performance calculations.

Education

  • 1971 - 1976
    University of Bristol
  • 1959 - 1963
    University of Salford

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Industry Focus. “Research”

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