AEM Seminar:
Plasma Tunnels for Hypersonics and Magnetoaerodynamics
Abstract: This
seminar will cover an overview of several newly commissioned plasma
tunnels for hypersonic applications as well as current and future
research studies in the Magnetoaerodynamics and Aerospace Plasmas
Laboratory at the University of Colorado Boulder, directed by Assistant
Professor Hisham Ali. The laboratory specializes in studying the physics
of aerospace plasmas and related applications, such as hypersonics. Key
laboratory capabilities include several unique radio- frequency (RF)
inductively coupled plasma (ICP) tunnel facilities designed and built
within the laboratory, spanning a range of input power levels up to
40kW. The facilities produce high-temperature supersonic ionized plasma
flows to simulate plasmas formed during high altitude hypersonic flight,
featuring table-top scale up to 5kW tunnels and larger scale up to 40kW
facilities, with full operation of the larger 40kW main facilities
achieved in late 2025 after an over three-year facility design, building
renovation, and equipment integration effort. The larger scale main
plasma tunnel facilities are driven by water-cooled RF ICP torches
operating at 40kW and 13.56MHz. In the context of RF ICP tunnels
for hypersonics, the combination of up to 40kW input power and
relatively high 13.56MHz frequency enable generation of chemically pure,
high enthalpy flows with relatively high ionization levels. These RF
ICP sources are then coupled to converging diverging nozzles and
water-cooled 1.5m x 1.5m vacuum chambers evacuated by a shared large
capacity mechanical vacuum pumping system, with a base pressure of
5x10-4 mbar and maximum volumetric pumping speed exceeding 20,000 m3/hr.
The resulting plasma jet discharge into the test vacuum chamber is a
continuous supersonic plasma tunnel ground test facility simulating an
ionized hypersonic plasma free-stream at high-altitude (low base
pressure), with temperatures exceeding several thousand degrees K. The
laboratory power supply, water-cooling, and vacuum systems are designed
such that all plasma tunnels can run simultaneously to enable higher
testing throughput, a unique capability. Overall, the facility is one of
less than five such high power inductively coupled plasma tunnel
facilities in US academia, and its uniquely high vacuum pumping capacity
is capable of maintaining lower chamber base pressures for simulating
high altitude hypersonic flight environments while also featuring a
control system to increase base pressure for simulating lower altitudes.
The laboratory includes access for various plasma, fluid, and thermal
diagnostics to facilitate hypersonics experimental investigations with a
unique focus on magnetohydrodynamics for hypersonics and
aerospace plasmas—magnetoaerodynamics.
Bio: Hisham
is an Assistant Professor in the Ann and H.J. Smead Department of
Aerospace Engineering Sciences at The University of Colorado Boulder and
the director of the Magnetoaerodynamics and Aerospace Plasmas
Laboratory. In addition, Hisham is concurrently affiliated as a
part-time casual Member of Technical Staff at The Aerospace Corporation
Colorado Springs, a Federally Funded Research and Development Center for
the United States Space Enterprise. Hisham earned a Bachelor of Science
in Aerospace Engineering with minors in Mathematics and Computer Based
Honors from The University of Alabama in May 2013 and earned his Master
of Science and Doctor of Philosophy in Aerospace Engineering from the
Georgia Institute of Technology in May 2015 and August 2019,
respectively.
Hisham’s current research interests are in magnetohydrodynamics, hypersonics, plasma physics, and planetary entry systems.
*Refreshments to follow in 209 Akerman Hall