NOZZLE FLOW INTO A VACUUM.
Abstract
Details are given of the numerical procedures required for the calculation of the flow from a supersonic axi-symmetric nozzle into a vacuum. The streamlines and density contours of the flow are computed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1967
- Accession Number
- AD0661180
Entities
People
- M. J. W. Gage
Organizations
- Royal Aircraft Establishment