Aerodynamic characteristics of a hypersonic parachute

Simple item page
dc.contributor.authorBoyd, E. A.
dc.date.accessioned2014-12-05T16:41:34Z
dc.date.available2014-12-05T16:41:34Z
dc.date.issued1961-11
dc.description.abstractNewtonian theory, both in the form of the Modified-Newtonian and the Newton- Busemann pressure laws, is used to find the shape, cloth area and drag of the axisymmetric canopy of a hypersonic parachute, whose only load-carrying fibres are longitudinal ones. As an example, an estimate is made of the size of canopy needed to give a drag of 20,000 lb. in flight at a Mach number of 10 at 100,000 feet altitude.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/8853
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCollege of Aeronautics Reportsen_UK
dc.relation.ispartofseries152en_UK
dc.relation.ispartofseriesCOA/152en_UK
dc.titleAerodynamic characteristics of a hypersonic parachuteen_UK
dc.typeReporten_UK

Files

Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
COA_Report_152_November_1961.pdf
Size:
2.8 MB
Format:
Adobe Portable Document Format
Download
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.79 KB
Format:
Item-specific license agreed upon to submission
Description:
Download

Collections

CoA. Reports