Add to ORKGA computer program is presented by which the effects of nonlinear suspension-system elastic characteristics on parachute inflation loads and motions can be investigated. A mathematical elastic model of suspension-system geometry is coupled to the planar equations of motion of a general vehicle and canopy. Canopy geometry and aerodynamic drag characteristics and suspension-system elastic properties are tabular inputs. The equations of motion are numerically integrated by use of an equivalent fifth-order Runge-Kutta technique
Although many sophisticated stability models of parachutes have appeared, advances are concentrated ...
Motion resembling that of a pendulum undergoing large-amplitude limit cycle oscillation was observed...
AbstractTo analyze the parachute dynamics and stability characteristics of precision airdrop system,...
A two-body computerized mathematical model is used to calculate planar dynamics of the LADT #3 and s...
The derivation of the differential equations of motion of a 3 Degrees of Freedom body joined to a 3 ...
The main focus is on the Computational fluid interaction of the effect of parachutes in use on stres...
A general theory on mathematical modeling of elastic parachute suspension lines during the unfurling...
The main focus is on the Computational fluid interaction of the effect of parachutes in use on stres...
Analytical calculations have considered the effects of 1) varying parachute system mass, 2) suspensi...
To analyze the parachute dynamics and stability characteristics of precision airdrop system, the flu...
AbstractA direct numerical modeling method for parachute is proposed firstly, and a model for the st...
The nonlinear differential equations of motion for a general parachute-riser-payload system are deve...
Includes bibliographical references (pages 53-54)This paper discusses the application of Finite Elem...
Digital computer rigid body simulation of impervious hemisphere and disk-gap-band parachute systems ...
Equations are presented which govern the dynamics of the lines-first parachute unfurling process, in...
Although many sophisticated stability models of parachutes have appeared, advances are concentrated ...
Motion resembling that of a pendulum undergoing large-amplitude limit cycle oscillation was observed...
AbstractTo analyze the parachute dynamics and stability characteristics of precision airdrop system,...
A two-body computerized mathematical model is used to calculate planar dynamics of the LADT #3 and s...
The derivation of the differential equations of motion of a 3 Degrees of Freedom body joined to a 3 ...
The main focus is on the Computational fluid interaction of the effect of parachutes in use on stres...
A general theory on mathematical modeling of elastic parachute suspension lines during the unfurling...
The main focus is on the Computational fluid interaction of the effect of parachutes in use on stres...
Analytical calculations have considered the effects of 1) varying parachute system mass, 2) suspensi...
To analyze the parachute dynamics and stability characteristics of precision airdrop system, the flu...
AbstractA direct numerical modeling method for parachute is proposed firstly, and a model for the st...
The nonlinear differential equations of motion for a general parachute-riser-payload system are deve...
Includes bibliographical references (pages 53-54)This paper discusses the application of Finite Elem...
Digital computer rigid body simulation of impervious hemisphere and disk-gap-band parachute systems ...
Equations are presented which govern the dynamics of the lines-first parachute unfurling process, in...
Although many sophisticated stability models of parachutes have appeared, advances are concentrated ...
Motion resembling that of a pendulum undergoing large-amplitude limit cycle oscillation was observed...
AbstractTo analyze the parachute dynamics and stability characteristics of precision airdrop system,...