Abstract
The experimental data on the convective heating of the nose surface of the model Mars Science Laboratory (MSL) Martian entry vehicle a in three-dimensional flow are numerically investigated in a wide Reynolds number range. It is shown that the application of the algebraic turbulence model of Baldwin-Lomax and the mixing model of Prandtl, together with the Reynolds-averaged Navier-Stokes equations, allows one to obtain a reasonable agreement with the experimental and calculated data of other authors.
Full Text 
Sign-in/Register to access full text options
Sign-in/Register to access full text options 
Published version (
Free)
Free) 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
