Methodology for Estimation of Shock Wave and Acoustic Loading of a Designed Rocket Block Equipped with an Aerospike Engine at the Landing Stage
Year: 2024
Type: article
Source: Russian Aeronautics
Authors: R. A. Peshkov, P. A. Tret’yakov
Institution: South Ural State University
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4406367707