39th Aerospace Sciences Meeting and Exhibit 2001
DOI: 10.2514/6.2001-355
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Modeling of radiation in Atlas plume-flow

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Cited by 7 publications
(9 citation statements)
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“…These results were presented in [20] and a paper has been prepared and submitted for publication [21].…”
Section: Discussionmentioning
confidence: 99%
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“…These results were presented in [20] and a paper has been prepared and submitted for publication [21].…”
Section: Discussionmentioning
confidence: 99%
“…This gives a qualitative description of the flow fields and shows how the different flight conditions affect the overall flow topology. The results have been used to compute the radiative emission from the Atlas-II flow fields to compare with emission measurements [19].…”
Section: Three-dimensioned Atlas-ii Plumesmentioning
confidence: 99%
“…Where 1 a n P P = represents the expansion ratio, 2 Ma , 2 P , 2 T and 2 u respectively stands for the Mach number, the pressure, the temperature and the velocity at the front part of Mach disk, and 3 Ma , 3 P , 3 T and 3 u are the counterpart parameters at the hinder part.…”
Section: A Simplified Three Region Flow Field Model Of Rocket Plumementioning
confidence: 99%
“…The detailed models adopted in Ref. [1][2][3] proceed from the combustion chamber of rocket motor, and build up a combustion model to acquire the gas parameters at the motor nozzle according to the component of propellant and its burning condition. Then the parameters, together with those of the atmosphere around, and the flying status of the rocket, are substituted as initial conditions into the plume flow field model as described by Navier-Stokes equations, to find the flow field parameter distribution to be substituted into rocket plume infrared radiation transmission equations for the exact infrared radiation of rocket plumes.…”
Section: Introductionmentioning
confidence: 99%
“…Also the studies by Lee et al [4,5] and Fu et al [6] present CFD models to simulate the missile launch from a canister in general or from a helicopter with the focus on the missile movement. Simulations of the exhaust plume from launcher rockets using CFD modelling were performed by Gusman et al [7], Alexeenko et al [8], Ebrahimi et al [9], and Vitkin et al [10]. The complex flow fields generated by missile propulsion systems are challenging for CFD simulations with Navier-Stokes flow solvers though.…”
Section: Introductionmentioning
confidence: 99%