Accession Number:

AD0661180

Title:

NOZZLE FLOW INTO A VACUUM.

Descriptive Note:

Technical rept.,

Corporate Author:

ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (ENGLAND)

Personal Author(s):

Report Date:

1967-01-01

Pagination or Media Count:

23.0

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

Subject Categories:

  • Aerodynamics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE