Analytical Evaluation of Box Wing Aircraft Aerodynamic Characteristics at Early Design Stages

被引：0

作者：

Karpovich E.A. ^{[1
]}

Liseitsev N.K. ^{[1
]}

机构：

[1] Moscow Aviation Institute, National Research University, Volokolamskoe sh. 4, Moscow

来源：

Russian Aeronautics | 2019年 / 62卷 / 03期

关键词：

aerodynamic characteristics; biplane; box wing; thin airfoil theory; vortex lattice method;

D O I：

10.3103/S1068799819030085

中图分类号：

学科分类号：

摘要：

The first-approach techniques for analytical evaluation of the airfoil shape and calculation of the aerodynamic coefficients for a box-wing aircraft are suggested. The reliability of the calculation results was estimated using FLZ code (the vortex lattice method). The comparison showed satisfactory convergence of coefficients for the clean configuration and some discrepancy for the take-off and landing configuration. © 2019, Allerton Press, Inc.

引用

页码：417 / 422

页数：5