Based on the finite volume method, the Navier-Stokes equation is used to calculate the aerodynamic heating of the two-dimensional spiral model. A new adaptive grid processing method is introduced for the heat loss quasi-problem problem in the traditional grid topology calculation. The numerical simulation is based on the ballistic data. Calculate the heat flow of the spiral model stagnation point. The CFD calculation results are compared with the traditional Fay-Riddell formula results to verify the feasibility and accuracy of the method.
Numerical Analysis of Aerodynamic Heating of Two-dimensional spiral model
2019-07-01
201094 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Numerical Analysis of Aerodynamic Heating on MUSES-C Reentry Capsule
British Library Conference Proceedings | 1996
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