301. Coherent Anti-Stokes Raman Scattering Temperature Measurements on an Air Breathing Ramjet Model
- Author
-
Adi Winandy, Sebastian Cordes, Hedwig Weisgerber, Eggert Magens, and Michael Fischer
- Subjects
Hypersonic speed ,Materials science ,nonequilibrium ,Nozzle ,Aerospace Engineering ,Non-equilibrium thermodynamics ,Thrust ,mean ,PDF ,Temperature measurement ,Spectral line ,Scattering ,Physics::Fluid Dynamics ,symbols.namesake ,Optics ,CARS ,Physics::Chemical Physics ,Raman ,Ramjet ,nozzle ,business.industry ,RMS(T) ,Anti-Stokes ,temperature ,ramjet ,hydrogen ,vibrational ,Physics::Space Physics ,symbols ,Coherent ,Atomic physics ,rotational ,business ,air-breathing ,Raman scattering - Abstract
Coherent anti-Stokes Raman scattering was used to measure nitrogen single-pulse spectra at the entrance and exit area of a thrust nozzle. Thermodynamic nonequilibrium effects were proved at the exit of the hypersonic nozzle, belonging to an air-breathing, hydrogen-combusting ramjet model. To determine the accurracy of extracted rotational and vibrational temperatures, additional laboratory experiments were performed. The nozzle expansion was characterized by wall pressure measurements
- Published
- 1999