The trajectory model for a subsonic fin-stabilized projectile at low angle of attack is typically a point-mass model (PMM). The disadvantage of this approach is the lack of prediction on the precision and the attitude of the projectile when hitting the target, because of a possible instability. The consideration of other forces and moments acting on the projectile in flight is an instructive step in the field of non-lethal ammunition trajectories
abstract: The goal of this thesis project was to build an understanding of supersonic projectile dyn...
International audienceAn aerodynamic analysis was initiated to understand the behavior of two spinni...
© 2012 Jonathan Brian Da CostaThe simulation of missile systems plays an important role in the devel...
peer reviewedNowadays, the trajectory model for a subsonic fin-stabilized projectile at low angle of...
The transition from inner to outer ballistics is a crucial part for the stability of the projectile....
A full six degrees of freedom (6-DOF) flight dynamics model is proposed for the accurate prediction ...
Sophisticated artillery munitions with guiding capabilities might be fin stabilised and thus deploym...
The paper presents the study of unguided rolling projectiles at varying Mach numbers using aerodyna...
International audiencePurposeThe present paper deals with weapon aerodynamics and aims to describe p...
The transition from inner to outer ballistics is a crucial part of the launch of a projectile from a...
International audienceThe present paper covers preliminary developments of a code which goal is to p...
It is well known that projectiles equipped with liquid payloads experience large destabilizingmoment...
International audienceThe present research investigates the flight dynamics modeling of a new class ...
Abstract--A case study of flow over a body of revolution was done in order to understand the variati...
An investigation at medium to high subsonic speeds has been conducted in the Langley low-turbulence ...
abstract: The goal of this thesis project was to build an understanding of supersonic projectile dyn...
International audienceAn aerodynamic analysis was initiated to understand the behavior of two spinni...
© 2012 Jonathan Brian Da CostaThe simulation of missile systems plays an important role in the devel...
peer reviewedNowadays, the trajectory model for a subsonic fin-stabilized projectile at low angle of...
The transition from inner to outer ballistics is a crucial part for the stability of the projectile....
A full six degrees of freedom (6-DOF) flight dynamics model is proposed for the accurate prediction ...
Sophisticated artillery munitions with guiding capabilities might be fin stabilised and thus deploym...
The paper presents the study of unguided rolling projectiles at varying Mach numbers using aerodyna...
International audiencePurposeThe present paper deals with weapon aerodynamics and aims to describe p...
The transition from inner to outer ballistics is a crucial part of the launch of a projectile from a...
International audienceThe present paper covers preliminary developments of a code which goal is to p...
It is well known that projectiles equipped with liquid payloads experience large destabilizingmoment...
International audienceThe present research investigates the flight dynamics modeling of a new class ...
Abstract--A case study of flow over a body of revolution was done in order to understand the variati...
An investigation at medium to high subsonic speeds has been conducted in the Langley low-turbulence ...
abstract: The goal of this thesis project was to build an understanding of supersonic projectile dyn...
International audienceAn aerodynamic analysis was initiated to understand the behavior of two spinni...
© 2012 Jonathan Brian Da CostaThe simulation of missile systems plays an important role in the devel...