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Measurement of the static and dynamic coefficients of a cross-type parachute in subsonic flowAn experimental parametric investigation of the aerodynamic qualities of cross-type parachutes was performed in a subsonic wind tunnel, using a new experimental technique. This investigation included the measurement of the static and dynamic aerodynamic coefficients, utilizing the measuring apparatus modified specifically for this type of testing. It is shown that the static aerodynamic coefficients of several configurations are in good agreement with available data, and assisted in validating the experimental technique employed. Two configuration parameters were varied in the static tests, the cord length and the canopy aspect ratio, with both parameters having a similar effect on the drag measurement, i.e., any increase in either of them increased the effective blocking area, and therefore the axial force.
Document ID
19910047560
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shpund, Zalman
(Technion - Israel Institute of Technology Haifa, United States)
Levin, Daniel
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 91-0871
Meeting Information
Meeting: AIAA Aerodynamic Decelerator Systems Technology Conference
Location: San Diego, CA
Country: United States
Start Date: April 9, 1991
End Date: April 11, 1991
Accession Number
91A32183
Distribution Limits
Public
Copyright
Other

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