학술논문

A preliminary characterization of parachute wake recontact
Document Type
Conference
Author
Source
Conference: 10. AIAA aerodynamic decelerator systems technical conference, Cocoa Beach, FL, USA, 18 Apr 1989; Other Information: Paper copy only, copy does not permit microfiche production
Subject
42 ENGINEERING PARACHUTES
EVALUATION
BOMBS
DATA ACQUISITION
EXPERIMENTAL DATA
FLOW MODELS
TURBULENCE
VELOCITY
WIND
DATA
INFORMATION
MATHEMATICAL MODELS
NUMERICAL DATA
WEAPONS 420200* -- Engineering-- Facilities, Equipment, & Techniques
Language
English
Abstract
A series of tests was conducted on a 10-ft.-diameter ringslot parachute with a geometric porosity of 20% to establish the conditions under which ''wake recontact'' occurs. The vertical helicopter drop tests covered a range of mass ratios from 0.5 to 3.0 and a range of Froude numbers from 70 to 400. Data consisted of velocity time histories obtained using a laser tracker and diameter time histories obtained from photometric data. A collapse parameter based on the ratio of the maximum parachute diameter to the subsequent minimum diameter was correlated with the mass ratio M/sub R/ and the Froude number Fr or equivalently with the initial to final velocity ratio V/sub o//V/sub t/. For large values of V/sub o//V/sub t/ the collapse parameter R/sub c/ appears to be a function of M/sub R/ alone. Non-dimensional opening time and ''collapse time'' data were also correlated with M/sub R/ and V/sub o//V/sub t/. 11 refs., 10 figs., 1 tab.