Measurement of scalar flowfield at exit of combustor sector using Raman diagnostics
By: Anil Gulati.
Contributors: AIAA
Publisher: American Institute of Aeronautics and Astronautics
Published: 1992
Place of publication: Washington, D. C
Number of pages: 10
Subjects: Aircraft engines; Combustion chambers; Raman spectroscopy
Notes: Includes bibliographical references: p. 9-10.

Source: AIAA/SAE/ASME/ASEE 28th Joint Propulsion Conference and Exhibit, July 6-8, 1992/Nashville, Tenn