Rocket Exhaust Plume Phenomenology

By F. S. Simmons. 2000

157 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Applied Mathematics, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/bf208d7438098f37b4937e2095379034db003559

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. Lijun Xu
2. Chang Liu

In Applied Mathematics

1. Lijun Xu
2. Chang Liu

In Computational Mechanics

1. Lijun Xu
2. Chang Liu
3. R. Haelterman

Citations in the corpus

• Hypersectral Imaging for Military and Security Applications: Combining Myriad Processing and Sensing Techniques (2019, background): “Understanding computational fluid dynamics models is a challenging task that combines rocket and engine type, propellant composition, chamber and nozzle parameters, burn time, flight mechanics, and atmospheric conditions [41], [43], [44].”
• Laser absorption spectroscopy for combustion diagnosis in reactive flows: A review (2019, background): “For some combustors such as the flat flame burner and the rocket propeller, the distributions of the combustion parameters over the cross-sections of the flame are rotationally symmetric, or, to some extent, can be simplified as rotationally symmetric (123, 124).”