English (United Kingdom)

https://curated-unify.zendy.io/wp-json/zendy-region/v1/featured_content/oa?rat=en

https://curated-unify.zendy.io/wp-json/zendy-region/v1/highlighted_journal/

Global: Zendy Plus annual

Presents the access of premium content as premium feature

Premium Content

Presents the keyphrase highlighting as premium feature

Keyphrase Highlighting

Presents the summarisation as premium feature

Summarisation

Insights

Presents the pdf analysis as premium feature

PDF Analysis

Presents the zaia usage as premium feature

ZAIA

Global: Zendy Plus monthly

Global: Zendy Tools annual

Global: Zendy Tools monthly

Global: Zendy Free Plan

The present paper contains the results of the aerodynamics and gas dynamics calculations of HB–1 standard ballistic model performed by the UST3D code. There were the following test cases for the numerical simulations. At first, the computations were conducted for the different Mach numbers at the various angles of attack. At second, the effect of the tetrahedron grid elements number on the flow field and aerodynamics coefficients was estimated. At last, the different approaches to the decay of discontinuity investigation were applied. The comparisons between the experimental data and results of calculations are also presented.

Application of the finite volume method for the standard ballistic model aerodynamics calculations