Open AccessRefining the aerodynamic moment of the missile based on flight test results
Author(s) -
В. Н. Акимов,
A. Kostyukov,
E. N. Kravchuk,
K. O. Rozantsev
Publication year - 2021
Publication title -
vestnik koncerna vko «almaz - antej»
Language(s) - English
Resource type - Journals
ISSN - 2542-0542
DOI - 10.38013/2542-0542-2021-4-47-56
Subject(s) - missile , aerodynamics , moment (physics) , convergence (economics) , flight test , aerospace engineering , pitching moment , computer science , computation , flight dynamics , software , trajectory , aeronautics , engineering , angle of attack , algorithm , physics , classical mechanics , astronomy , economics , programming language , economic growth
This research paper is intended to refine the aerodynamic moment of the missile based on an analysis of flight tests and results of gas dynamics software computations. The paper compares mathematical simulation results with flight test data in order to demonstrate an improved convergence due to the proposed refinement.