俄罗斯空气动力研究所中心学报
每年出版 6 期
ISSN 打印: 1948-2590
ISSN 在线: 1948-2604
METHOD OF COMPUTATION OF AERODYNAMIC CHARACTERISTICS OF THE WING–TAIL CONFIGURATION IN TRANSONIC CRUISE FLIGHT
卷 49,
册 6, 2018,
pp. 611-618
DOI: 10.1615/TsAGISciJ.2018029236
摘要
The method of computation of transonic flow over a swept wing based on the full-potential equation is extended to the classical wing-tail configuration. It is assumed that a high-aspect-ratio wing affects the tail located behind it only by the vortex sheet coming off the wing trailing edge. The effect of the tail on the wing is neglected. Comparison of the developed technique with the vortex-lattice method and with the method of solution of Navier-Stokes equations is implemented for a text configuration.
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