A SIMPLE METHOD OF CALCULATING A LAVAL NOZZLE,

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Abstract:

The paper presents a simple method of constructing a Laval nozzle to assure a plane-parallel supersonic flow. A simplified method is given for calculating the initial velocity distribution of the sonic and supersonic portions of the nozzle and formulas are introduced together with curve equations for calculating the compensating section of the nozzle wall. An example of the nozzle construction formulas is given in order of their calculation. Author

Author(s):
Dorfman, A. Sh.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Edited trans. of Akademiya Nauk URSR, Kiev. Instytut Teploenergetyky. Sbornik Trudov, v14 p26-31 1958, by M. Olaechea.
Annotation:
A simple method of calculating a laval nozzle--Translation.
Pagination:
0011

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-HT-23-414-69
Project Number(s):
FTD-6040313
 Subject Terms
Communities of Interest:
Air Platforms
Descriptor(s):
(*LAVAL NOZZLES, SUPERSONIC CHARACTERISTICS), (*NOZZLE GAS FLOW, LAVAL NOZZLES), VELOCITY, DISTRIBUTION, DESIGN, MATHEMATICAL ANALYSIS, USSR
Field(s)/Group(s):
Aerodynamics, Fluid Mechanics
Keyword(s):
TRANSLATIONS
Report Date:
1969 Dec 11