CALCULATIONS FOR THE DESIGN OF NOZZLES.

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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

Author(s):
Dodd, K. N. ; Piggott, B. A. M. ; Day, B. P.
Author Organization(s):
ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (UNITED KINGDOM)
Descriptive Note:
Technical rept.,
Annotation:
Calculations for the design of nozzles.
Pagination:
0014

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
RAE-TR-64021
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*ROCKET NOZZLES, AEROSPACE CRAFT, AXISYMMETRIC FLOW, ATTITUDE CONTROL SYSTEMS, BOUNDARY LAYER, CONFIGURATIONS
Report Date:
1964 Oct 01