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NUMERICAL SIMULATION OF SUBSONIC AND TRANSONIC FLOW AROUND THIN SHELLS

Authors :
A. A. Dyadkin
A. Yu. Lutsenko
D. K. Nazarova
Source :
Naučnyj Vestnik MGTU GA, Iss 223, Pp 45-50 (2016)
Publication Year :
2016
Publisher :
Moscow State Technical University of Civil Aviation, 2016.

Abstract

Numerical simulation of flow around a nose fairing half of a launch vehicle was carried out, aerodynamic characteristics of the model were calculated at subsonic and transonic flow velocities, the flow patterns around a thin shell were analyzed.

Subjects

Subjects :
jettisonable elements
launch vehicle
aerodynamic characteristics
numerical simulation
nose fairing
TL1-4050
Motor vehicles. Aeronautics. Astronautics

Details

Language :
Russian
ISSN :
25420119 and 20790619
Issue :
223
Database :
OpenAIRE
Journal :
Naučnyj Vestnik MGTU GA
Accession number :
edsair.doajarticles..3ba48c83dc5e401d6997708643dd333d

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