Pregled bibliografske jedinice broj: 14724
A turbulent flow shape optimization method for nozzle design
A turbulent flow shape optimization method for nozzle design // PVP-Vol. 377-2 Computational Technologies for Fluid/Thermal/Structural/Chemical Systems with Industrial Applications / Klein, Chris R ; Kawano, Satoyuki ; Kudriavtsev, Vladimir V. (ur.).
San Diego (CA), Sjedinjene Američke Države: American Society of Mechanical Engineers (ASME), 1998. str. 87-92 (predavanje, međunarodna recenzija, cjeloviti rad (in extenso), znanstveni)
CROSBI ID: 14724 Za ispravke kontaktirajte CROSBI podršku putem web obrasca
Naslov
A turbulent flow shape optimization method for nozzle design
Autori
Mrša, Zoran
Vrsta, podvrsta i kategorija rada
Radovi u zbornicima skupova, cjeloviti rad (in extenso), znanstveni
Izvornik
PVP-Vol. 377-2 Computational Technologies for
Fluid/Thermal/Structural/Chemical Systems with Industrial Applications
/ Klein, Chris R ; Kawano, Satoyuki ; Kudriavtsev, Vladimir V. - : American Society of Mechanical Engineers (ASME), 1998, 87-92
Skup
The 1998 ASME/JSME Joint Pressure Vessels and Piping Conference
Mjesto i datum
San Diego (CA), Sjedinjene Američke Države, 26.07.1998. - 30.07.1998
Vrsta sudjelovanja
Predavanje
Vrsta recenzije
Međunarodna recenzija
Ključne riječi
shape optimization; nozzle design; genetic algorithm
Sažetak
The paper presents a shape optimization method for nozzle design. Using commercial turbulent flow modeling software FLUENT and conjugate gradient method and genetic algorithm alternately, the energy losses, defined as the difference of total mechanical energy flux in inflow and outflow cross-sections, are minimized in the set of admissible nozzle shapes. The shape of the nozzle is parameterized by cubic Bezier spline, the coordinates of control points being optimizing parameters. The macro code has been developed that couples all three elements of the modeling and optimization process: preBFC automatic mesh generator, FLUENT turbulent k-e flow simulator and conjugate gradient and genetic algorithm optimization module. The analysis of the numerical results of the nozzle shape optimization leads to the main conclusion that a minimum number of two parameters are enough for the desired accuracy of the solution. Compared to the circular arc, the optimum shape is more concave, starting and ending with smaller curvature and with greater curvature in the middle part.
Izvorni jezik
Engleski
Znanstvena područja
Strojarstvo