Injection and Mixing Processes in High-Pressure Liquid Oxygen/Gaseous Hydrogen Rocket Combustors

By W. Mayer, A. Schik, M. Schaffler, H. Tamura. 2000

147 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/1496261a7c9f409e9d31502a7a6cf491772f3079

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Vigor Yang
2. Nana Zong
3. Matthew P. Juniper
4. S. Candel
5. R. Sujith
6. T. Schuller
7. Lipika Kabiraj

In Computational Mechanics

1. Nana Zong
2. Matthew P. Juniper
3. Vigor Yang
4. S. Candel
5. J. Hussong
6. R. Branam
7. R. Sujith
8. Thierry Poinsot

Citations in the corpus

• CRYOGENIC FLUID JETS AND MIXING LAYERS IN TRANSCRITICAL AND SUPERCRITICAL ENVIRONMENTS (2006, methodology): “The studies included injection of liquid nitrogen and coaxial injection of liquid nitrogen and gaseous helium into vessels preconditioned with high-pressure gaseous nitrogen (Branam and Mayer, 2003; Chehroudi et al., 2002a, 2002b; Mayer et al., 2000; Mayer and Smith, 2004; Oschwald and Schik, 1999).”
• STRUCTURE AND DYNAMICS OF CRYOGENIC FLAMES AT SUPERCRITICAL PRESSURE (2006, background): “…1995, 1996, 1998; Juniper et al., 2000, 2001a, 2001b; Kendrick et al., 1998, 1999; Snyder et al., 1997; Tripathi, 2001) Another set of results are described in Mayer et al. (1996, 1998, 2000, 2001), and Mayer and Tamura (1996), but these studies pertain to a different range of injection conditions.”
• Raman Measurements of Cryogenic Injection at Supercritical Pressure (2003, methodology): “The set-up is described in more detail in the previous campaigns and can be found in [ 4 ].”