Heating Rate of the Driven Gas in a Hartmann-Sprenger Tube
Author:
Affiliation:
1. Institut de Mecanique des Fluides, Marseille, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.60537
Reference8 articles.
1. 'Phillips, B. R. and Pavli, A. J. "Resonance tube ignition of hydrogen-oxygen mixtures,'* TN D-6354, May 1971, NASA.
2. A Fluidic Sounding Rocket Motor Ignition System
3. Etude des phenomenes thermiques dans un tube de Hartmann-Sprenger
4. Finite-amplitude and diffusive effects in acoustics: a report on EUROMECH 23
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