Autor: |
Sochnev, A. V., Aleksandrov, Yu. B., Ziganshin, B. R. |
Zdroj: |
Russian Aeronautics; Apr2021, Vol. 64 Issue 2, p256-261, 6p |
Abstrakt: |
The results of numerical simulation at atmospheric pressure and air motion in the range of 40–1600 Reynolds numbers are presented. It makes possible to estimate aerodynamic losses during measuring the target impulse by the ballistic pendulum method. Results from numerical simulation are compared with experimental data. [ABSTRACT FROM AUTHOR] |
Databáze: |
Complementary Index |
Externí odkaz: |
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