Theory of supersonic flow in nozzles discussed, emphasis being placed on physical rather than mathematical point of view; methods, both graphic and analytic, for designing nozzles described together with discussion of design factors; analysis of given nozzle shapes to determine velocity distribution and possible existence of shock waves is considered.
Supersonic nozzle design
Nat Advisory Committee Aeronautics -- Tech Note
1948
34 pages
Bibliography
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
TIBKAT | 1948
|NTRS | 1948
|AIAA | 2005
|NTIS | 1990
|TIBKAT | 1967
|