Off-Body Pressure Measurements using Femtosecond CARS

Measurements in NASA's wind tunnels generally consist of force and moment and on-body measurements like surface pressure, surface deflection or heat transfer to the surface. Detailed off-body measurements are needed to understand complex wind tunnel flows and to provide data to validate high-fidelity computational models. Most existing techniques capable of measuring detailed off-body flows, for example, particle image velocimetry, require particle or gas seeding which is not possible in many of NASA's tunnels. In this project, two techniques utilizing new femtosecond laser technology will be investigated. Both techniques show promise of measuring multiple parameters quantitatively in unseeded wind tunnel flows. The femtosecond laser electronic excitation and tagging (FLEET) technique can measure velocity and potentially pressure and temperature simultaneously. The femtosecond coherent anti-Stokes Raman spectroscopy (FS-CARS) technique can measure pressure, temperature and species concentrations. The two techniques have relative advantages and limitations that will be explored. The objective of this research project is to leverage recent advancements in laser technology and recent discoveries in academia to discover and apply new ways of measuring aerospace flows. In particular, methods of measuring the gas velocity, pressure, temperature and concentration will be developed. The two different measurement techniques share a common femtosecond laser technology and can be used separately or together to measure multiple gas properties simultaneously in wind tunnel flows and possibly in flight. In this project, we are extending the ability of FLEET to measure multiple parameters such as pressure and temperature simultaneous with velocity. These additional parameters will be obtained by observing and interpreting the amplitude and spectrum of the FLEET signal. The main novelty of the proposed work is that FLEET should allow velocity to be measured in several facilities where velocity cannot be curren More »