Parachute flying physical model and inflation simulation analysis

Yihua Cao; Hong Xu

doi:10.1108/00022660410526079

Parachute flying physical model and inflation simulation analysis

Yihua Cao^*
, Hong Xu

^*Corresponding author for this work

School of Aeronautic Science and Engineering

Beihang University

Research output: Contribution to journal › Article › peer-review

4 Scopus citations

Abstract

By means of establishing parachute's flying physical model, four methods (i.e. tiny segment analysis method, inflating distance method, moment method and simulating canopy shape method) are adopted to analyze and calculate the variations of canopy shape and the parameters of parachute inflation. The results are simply analyzed, and the figures of all the results are compared.

Original language	English
Pages (from-to)	215-220
Number of pages	6
Journal	Aircraft Engineering and Aerospace Technology
Volume	76
Issue number	2
DOIs	https://doi.org/10.1108/00022660410526079
State	Published - 2004

Keywords

Dynamics
Motion
Simulation

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10.1108/00022660410526079

Cite this

@article{12920eb99fb9452db0e2ae190b51fbb5,

title = "Parachute flying physical model and inflation simulation analysis",

abstract = "By means of establishing parachute's flying physical model, four methods (i.e. tiny segment analysis method, inflating distance method, moment method and simulating canopy shape method) are adopted to analyze and calculate the variations of canopy shape and the parameters of parachute inflation. The results are simply analyzed, and the figures of all the results are compared.",

keywords = "Dynamics, Motion, Simulation",

author = "Yihua Cao and Hong Xu",

year = "2004",

doi = "10.1108/00022660410526079",

language = "英语",

volume = "76",

pages = "215--220",

journal = "Aircraft Engineering and Aerospace Technology",

issn = "1748-8842",

publisher = "Emerald Publishing",

number = "2",

}

TY - JOUR

T1 - Parachute flying physical model and inflation simulation analysis

AU - Cao, Yihua

AU - Xu, Hong

PY - 2004

Y1 - 2004

N2 - By means of establishing parachute's flying physical model, four methods (i.e. tiny segment analysis method, inflating distance method, moment method and simulating canopy shape method) are adopted to analyze and calculate the variations of canopy shape and the parameters of parachute inflation. The results are simply analyzed, and the figures of all the results are compared.

AB - By means of establishing parachute's flying physical model, four methods (i.e. tiny segment analysis method, inflating distance method, moment method and simulating canopy shape method) are adopted to analyze and calculate the variations of canopy shape and the parameters of parachute inflation. The results are simply analyzed, and the figures of all the results are compared.

KW - Dynamics

KW - Motion

KW - Simulation

UR - https://www.scopus.com/pages/publications/1842586790

U2 - 10.1108/00022660410526079

DO - 10.1108/00022660410526079

M3 - 文章

AN - SCOPUS:1842586790

SN - 1748-8842

VL - 76

SP - 215

EP - 220

JO - Aircraft Engineering and Aerospace Technology

JF - Aircraft Engineering and Aerospace Technology

IS - 2

ER -

Parachute flying physical model and inflation simulation analysis

Abstract

Keywords

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