TY - JOUR
T1 - Analysis of the flow field of carrier-based aircraft exhaust jets impact on the flight deck
AU - Kuizhi, Yue
AU - Yicheng, Sun
AU - Hu, Liu
AU - Weigang, Guo
N1 - Publisher Copyright:
© The Korean Society for Aeronautical & Space Sciences.
PY - 2015
Y1 - 2015
N2 - In order to provide some references for suitability of carrier-based aircrafts, this paper studies the flow field of exhaust jets and its impact on the flight deck. The geometrical models of aircraft carrier and carrier-based aircrafts are firstly built, on which unstructured tetrahedral meshes are generated for numerical analysis. Then, this paper simulates the flow field of exhaust jets to evaluate its impact on the Jet Blast Deflector (JBD) and the flight deck, when four carrier-based aircrafts are ready to start off in the bow. The standard k-ε equations, three-dimension N-S equations and the Computational Fluid Dynamics (CFD) theory are used in the analysis process. To solve the equations, the thermal coupling of the wind and the jet flow are also considered. The velocity and temperature distributions are provided with the simulation of the CFD software, FLUENT. The results indicate that: (1) this analytical method can be used to simulate aerodynamic problems with complex geometrical models, and the results are of high reliability; (2) the safety working area, the installation scheme of the JBD and the arrangement of the take-off position can be optimized through analysis.
AB - In order to provide some references for suitability of carrier-based aircrafts, this paper studies the flow field of exhaust jets and its impact on the flight deck. The geometrical models of aircraft carrier and carrier-based aircrafts are firstly built, on which unstructured tetrahedral meshes are generated for numerical analysis. Then, this paper simulates the flow field of exhaust jets to evaluate its impact on the Jet Blast Deflector (JBD) and the flight deck, when four carrier-based aircrafts are ready to start off in the bow. The standard k-ε equations, three-dimension N-S equations and the Computational Fluid Dynamics (CFD) theory are used in the analysis process. To solve the equations, the thermal coupling of the wind and the jet flow are also considered. The velocity and temperature distributions are provided with the simulation of the CFD software, FLUENT. The results indicate that: (1) this analytical method can be used to simulate aerodynamic problems with complex geometrical models, and the results are of high reliability; (2) the safety working area, the installation scheme of the JBD and the arrangement of the take-off position can be optimized through analysis.
KW - Aircraft carrier
KW - Carrier-based aircraft
KW - Computational fluid dynamics (CFD)
KW - Numerical simulation
KW - Thermal coupling
UR - https://www.scopus.com/pages/publications/84926017327
U2 - 10.5139/IJASS.2015.16.1.1
DO - 10.5139/IJASS.2015.16.1.1
M3 - 文章
AN - SCOPUS:84926017327
SN - 2093-274X
VL - 16
SP - 1
EP - 7
JO - International Journal of Aeronautical and Space Sciences
JF - International Journal of Aeronautical and Space Sciences
IS - 1
ER -