If you think lighting a match on a windy day is hard, consider trying to light the flame in the combustion chamber of a hypersonic jet engine and keeping it lit. At the speeds hypersonic jets attain, the air moving through their engines is traveling many times faster than a Category 5 hurricane.
This year, the Air Force Office of Scientific Research joined forces with the National Science Foundation in awarding mechanical and aerospace engineering Professor Harsha Chelliah a $1.5 million grant to expand the validity of turbulence models that researchers use to predict high-speed reacting flows in hypersonic engines.
“The ultimate goal is to find ways to stabilize combustion over a shorter distance by premixing the air and fuel, better control of turbulence and mixing with vitiated gases in recirculation regions,” Chelliah says. “By reducing the overall length of the combustor, we will be able to decrease overall engine weight, and increase the payload.
This is the first time the two agencies have come together on a project of this size. The Air Force is interested in the military applications of this work, while the NSF is interested in the fundamental turbulence-chemistry interactions, which can be applied to many civilian applications.
A Record of Excellence in Hypersonic Propulsion
This grant is the latest in a series of awards that has placed the Engineering School at the forefront of an international effort to make hypersonic flight a reality. Six years ago, Professor James McDaniel secured a $9 million grant from NASA and AFOSR to establish the National Center for Hypersonic Combined Cycle Propulsion. NASA and AFOSR funded only three groups from among the 26 university and industry teams submitting preliminary proposals. In addition to Daniels, the winning team included Chelliah, Associate Professor Christopher Goyne and researchers from 10 other universities, national labs and corporations.
Since that time, the AFOSR has called on McDaniel and his colleagues to consider ways to reduce the size and weight of the scramjet engine, which powers hypersonic flight. In addition to this latest grant, AFOSR awarded Chelliah a $2.2 million grant in 2012 to explore a viable catalytic cooling system that uses a scramjet’s own fuel as a coolant. A traditional liquid coolant system capable of controlling temperatures of this magnitude would be prohibitively heavy.
Managing Turbulence
The challenge for Chelliah and his team, which includes Goyne and Senior Scientist Robert Rockwell, is that airflow inside the UVA scramjet engine test facility is moving extremely fast, from between Mach 0.6 to Mach 1.5 At these velocities it takes just 400 microseconds to burn the fuel/air mixture. Understanding the fundamental modes of turbulence-flame interactions under these conditions is critical.
The researchers at UVA, along with partners at NASA Langley and George Washington University, will focus on the experimental side of the project, trying to raise the limits of spatial resolution to 50 microns using nonintrusive laser-based diagnostic techniques. Researchers at North Carolina State University and Sandia National Laboratory will handle the computational and modeling side, attempting to produce a corresponding or higher level of resolution while covering larger domains than were previously possible. “We are trying to get down to the most basic scale of turbulent energy dissipation and feedback,” Chelliah says. “That way we will minimize uncertainties involved in making predictions about how to control it.”
One advantage Chelliah and his colleagues have is access to UVA’s Aerospace Research Laboratory, one of the few laboratories in the nation capable of reproducing the velocities found inside scramjet engines. They are also able to use NASA Langley’s 3-D printing facility, which will enable Chelliah’s team to test superalloy combustor geometries with different aspect ratios. “I am very excited about this opportunity,” Chelliah says. “It will help us reach our conclusions that much faster because we will be able to move back and forth between computational and experimental findings.”