The stresses occurring in the cloth of an opening parachute and at steady state are calculated. The method is based on assumed instantaneous and steady state shapes and related pressure distributions. It is general and may be applied to any type and size of canopy built out of solid cloth. The presented analysis is limited to canopies constructed of triangular gores, but can be extended to other gore patterns. A numerical calculation is made for the Solid Flat, Circular Parachute during the opening and at steady state."February 1965."Includes bibliograpical references (page 42).The stresses occurring in the cloth of an opening parachute and at steady state are calculated. The method is based on assumed instantaneous and steady state shapes ...
The main focus is on the Computational fluid interaction of the effect of parachutes in use on stres...
The main focus is on the Computational fluid interaction of the effect of parachutes in use on stres...
A technique for the aeroelastic solution of parachute decelerators is presented in this work. The me...
Includes bibliographical references (pages 53-54)This paper discusses the application of Finite Elem...
This paper presents a more accurate approximation of the mathematical relationship between riser ten...
The parachute decelerator system for the upcoming Mars Science Lab (MSL) mission will be designed to...
,SecCutry classilfcation of title. body of Abstract Alnd iide•xe,,,.dnnotatlhm nlut be entered when ...
Includes bibliographical references (page 33)An analytical method of the prediction of internal load...
We are honored to dedicate this paper to Charles Steele and to the memory of Marie-Louise Steele. Ch...
A direct numerical modeling method for parachute is proposed firstly, and a model for the star-shape...
AbstractA direct numerical modeling method for parachute is proposed firstly, and a model for the st...
Free-body tests were made in the Langley spin tunnel to determine drag coefficients for 1.07-meter-d...
Computational fluid dynamic studies of 3-D, fixed geometry, gore-shaped parachute canopies are prese...
The extra-large parachutes were different from the common parachutes because of their size and openi...
In this work, the authors continue researching issues related to fatigue of aircraft structures made...
The main focus is on the Computational fluid interaction of the effect of parachutes in use on stres...
The main focus is on the Computational fluid interaction of the effect of parachutes in use on stres...
A technique for the aeroelastic solution of parachute decelerators is presented in this work. The me...
Includes bibliographical references (pages 53-54)This paper discusses the application of Finite Elem...
This paper presents a more accurate approximation of the mathematical relationship between riser ten...
The parachute decelerator system for the upcoming Mars Science Lab (MSL) mission will be designed to...
,SecCutry classilfcation of title. body of Abstract Alnd iide•xe,,,.dnnotatlhm nlut be entered when ...
Includes bibliographical references (page 33)An analytical method of the prediction of internal load...
We are honored to dedicate this paper to Charles Steele and to the memory of Marie-Louise Steele. Ch...
A direct numerical modeling method for parachute is proposed firstly, and a model for the star-shape...
AbstractA direct numerical modeling method for parachute is proposed firstly, and a model for the st...
Free-body tests were made in the Langley spin tunnel to determine drag coefficients for 1.07-meter-d...
Computational fluid dynamic studies of 3-D, fixed geometry, gore-shaped parachute canopies are prese...
The extra-large parachutes were different from the common parachutes because of their size and openi...
In this work, the authors continue researching issues related to fatigue of aircraft structures made...
The main focus is on the Computational fluid interaction of the effect of parachutes in use on stres...
The main focus is on the Computational fluid interaction of the effect of parachutes in use on stres...
A technique for the aeroelastic solution of parachute decelerators is presented in this work. The me...