Dr. Gary Flandro
Boling Chair of Excellence in Space Propulsion
Professor of Aerospace Engineering
Ph.D., California Institute of Technology, 1967
Dr. Flandro is the first professor to fill the million-dollar Edward J. and Carolyn P. Boling Chair of Excellence in Space Propulsion at UTSI. His research interests include acoustics, aerodynamics, rocket propulsion, flight mechanics and performance, hypersonic aerodynamics, propulsion, and vehicle design. He is the discoverer of the multi-planet “Grand Tour” mission opportunity that utilized gravity assist of the space craft (ultimately the Voyager) to explore the four major outer planets of the solar system.
Research projects include application of computational fluid dynamics methods in solid rocket motor design, nonlinear combustion instability, effects of vorticity transport in unsteady rocket flows, effects of hypersonic vehicle flight attitude on scramjet thrust vector, flow-driven pressure oscillations in large segmented rockets, and dynamics of slag motion in spinning combustion chambers.
Planned research includes: application of hybrid low- thrust systems for manned interplanetary space flight, development of efficient, low-cost hybrid rocket motor thrust chambers, flame zone physicochemistry in solid rocket instability, predictive algorithm for nonlinear rocket instability, and effects of vehicle flexibility on hypersonic vehicle integrated propulsion system performance.
Nonlinear Combustion Instability
Effects of Vorticity Transport in unsteady rocket flows
Effects of hypersonic vehicle flight altitude on scramjet thrust vector
Flow-driven pressure oscillations in large segmented rockets
Dynamics of slag motion in spinning combustion chambers
Planned Research Topics
Application of hybrid low-thrust systems for manned interplanetary space flight
Development of efficient, low-cost hybrid rocket motor thrust chamber
Flame zone physicochemistry in solid rocket instability
Predictive algorithm for nonlinear rocket instability
Effects of vehicle flexibility on hypersonic vehicle integrated propulsion system performance
Compressible Flow I
Compressible Flow II
Rocket Propulsion I
Rocket Propulsion II