DocumentCode :
3230712
Title :
The investigation of the power characteristics of two-dimensional asymmetric nozzles
Author :
Zudov, Vladimir N. ; Lokotko, Anatoliy V.
Author_Institution :
Inst. of Theor. & Appl. Mech., Novosibirsk, Russia
fYear :
1997
fDate :
29 Sep-2 Oct 1997
Firstpage :
163
Lastpage :
173
Abstract :
A series of works on the construction of optimal supersonic 2D asymmetric nozzles and on the investigation of their off-design regimes was carried out. The variation problem of the design of the supersonic 2D asymmetric nozzles with maximum thrust at given lift power and given size limitations was solved. The method of characteristics was used. Structures of flow and power characteristics in nozzles are numerically investigated at transonic and supersonic speeds of external flow. Power characteristics and three-dimensional phenomena of 2D asymmetric nozzles were experimentally and numerically studied
Keywords :
Mach number; aircraft testing; nozzles; stagnation flow; supersonic flow; wind tunnels; external flow; lift power; off-design regimes; power characteristics; size limitations; supersonic nozzles; three-dimensional phenomena; thrust; transonic speeds; two-dimensional asymmetric nozzles; Aircraft; Atmosphere; Data visualization; Engines; Image motion analysis; Metalworking machines; Numerical simulation; Optical films; Testing; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 1997. ICIASF '97 Record., International Congress on
Conference_Location :
Pacific Grove, CA
Print_ISBN :
0-7803-4167-8
Type :
conf
DOI :
10.1109/ICIASF.1997.644678
Filename :
644678
Link To Document :
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