Accession Number:

AD0457270

Title:

CALCULATIONS FOR THE DESIGN OF NOZZLES.

Descriptive Note:

Technical rept.,

Corporate Author:

ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (UNITED KINGDOM)

Personal Author(s):

• Dodd, K. N.
• Piggott, B. A. M.
• Day, B. P.

Report Date:

1964-10-01

Pagination or Media Count:

14.0

Abstract:

Details are given of the numerical procedures required in the design of an axially-symmetric nozzle. A velocity distribution along the axis of symmetry is assumed to be given and from this, a characteristic network is used to determine the isentropic core boundary after which a boundary layer calculation gives the shape of the nozzle itself. Author

Descriptors:

• *ROCKET NOZZLES
• AEROSPACE CRAFT
• AXISYMMETRIC FLOW
• ATTITUDE CONTROL SYSTEMS
• BOUNDARY LAYER
• CONFIGURATIONS

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE