43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Amp;amp; Exhibit 2007
DOI: 10.2514/6.2007-5501
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A Numerical Model for Supercritical Flow in Rocket Engine Applications

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Cited by 1 publication
(2 citation statements)
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“…4 For this reason in the present study computations are made by a CFD solver which has been developed in Ref. 3, and is able to deal with compressible fluids whose behavior is represented by a generic equation of state. In particular, the Reynolds Averaged Navier-Stokes equations are solved by a Godunov-type finite volume scheme which is second-order accurate in space and third-order accurate in time.…”
Section: Methodsmentioning
confidence: 99%
See 1 more Smart Citation
“…4 For this reason in the present study computations are made by a CFD solver which has been developed in Ref. 3, and is able to deal with compressible fluids whose behavior is represented by a generic equation of state. In particular, the Reynolds Averaged Navier-Stokes equations are solved by a Godunov-type finite volume scheme which is second-order accurate in space and third-order accurate in time.…”
Section: Methodsmentioning
confidence: 99%
“…The reasons for choosing MBWR equation of state have been presented in Ref. 3. Here it is only reminded that it shows high accuracy to determine the correct pressure-volume-temperature behavior of a fluid and to compute specific heat at constant pressure, speed of sound, and internal energy.…”
Section: Transcritical Fluid Flow In Rocket Enginesmentioning
confidence: 99%