Add to ORKGThe ballistic missile model analysed in this paper presents a stringer type fuselage having 10 control surfaces, 8 directional surfaces to execute turns and 2 to execute manoeuvers for changing the angle of attack, but also 4 direction stabilisers. In this paper a CFD simulation was carried out on ballistic missile with a new structure for determining the flight performance and the aerodynamic configuration. It was also performed a finite element analysis of the ballistic missile and the results obtained allowed to precisely determine the areas where the stress is greatest and where is necessary to provide several measures to increase the structure’s rigidity, to protect it from temperature and pressure
At present ship to air missile is the main force of anti-missile. The warhead damage element’ impact...
Approved for public release; distribution is unlimited. 20001018 006 The findings in this report are...
The stress problem of Prithvi missile wing is investigated .\ud The analysis is carried out by the f...
This paper presents modification of the existing guided missile which was done by replacing the exis...
Wind tunnel test results of an Anti-Tank Missile model with five different warheads are presented in...
Designing a ballistic missile flight depends on the mission and the stress to which the missile is s...
The wing of missile can be considered as an effective factor for determination of lift to drag ratio...
Abstract CFD examples at ADD are introduced to show their variety at its application in the course o...
Missile fins or wings exposed to different coupled aerodynamic loads during the mission or flight at...
© 2012 Jonathan Brian Da CostaThe simulation of missile systems plays an important role in the devel...
The aerodynamics controlling performance of a missile depends a lot on its fins and their configurat...
In this thesis, shroud separation on generic missile is performed by using the Computational Fluid D...
During the flight of missiles, depending on the flight conditions, rotation of missiles around its c...
Attention in this work is focused on aerodynamic heating and aero-thermo-mechanical analysis of f...
This study focuses on the numerical simulation of supersonic flows around a missile with lattice win...
At present ship to air missile is the main force of anti-missile. The warhead damage element’ impact...
Approved for public release; distribution is unlimited. 20001018 006 The findings in this report are...
The stress problem of Prithvi missile wing is investigated .\ud The analysis is carried out by the f...
This paper presents modification of the existing guided missile which was done by replacing the exis...
Wind tunnel test results of an Anti-Tank Missile model with five different warheads are presented in...
Designing a ballistic missile flight depends on the mission and the stress to which the missile is s...
The wing of missile can be considered as an effective factor for determination of lift to drag ratio...
Abstract CFD examples at ADD are introduced to show their variety at its application in the course o...
Missile fins or wings exposed to different coupled aerodynamic loads during the mission or flight at...
© 2012 Jonathan Brian Da CostaThe simulation of missile systems plays an important role in the devel...
The aerodynamics controlling performance of a missile depends a lot on its fins and their configurat...
In this thesis, shroud separation on generic missile is performed by using the Computational Fluid D...
During the flight of missiles, depending on the flight conditions, rotation of missiles around its c...
Attention in this work is focused on aerodynamic heating and aero-thermo-mechanical analysis of f...
This study focuses on the numerical simulation of supersonic flows around a missile with lattice win...
At present ship to air missile is the main force of anti-missile. The warhead damage element’ impact...
Approved for public release; distribution is unlimited. 20001018 006 The findings in this report are...
The stress problem of Prithvi missile wing is investigated .\ud The analysis is carried out by the f...