1) wing/body/pylon/nacelle interference
翼身组合体/短舱/挂架干扰
2) Wing/body/Pylon/Nacelle configuration
翼/身/架/舱组合体
3) wing-body-pylon-nacelle configurations
机翼-机身-吊架-短舱组合体
4) wingbodystore configuration
翼身外挂物组合体
5) wing-body interference
翼身干扰
1.
, the ratios of local normal-force coefficient to its equivalent-circle one) and the correcting coefficients of wing-body interference factor.
提出了飞行器任意形状截面表观面积的数值计算模型和方法,从而求解非圆因子(即非圆剖面与当量圆剖面局部法向力系数之比)和翼身干扰因子的修正系数。
6) wing-body combination
翼-身组合体
1.
Two computed models and a numerical method based on nonlinear discrete vortex method are presented to simulate the vortex flow about wing-body combinations.
论述了用非线性离散涡法来模拟大迎角下翼－身组合体涡流绕流的计算模型及计算方法；给出了一个典型翼－身组合体的涡流流态计算结果及其非线性气动特性和截面压强（或载荷）分布。
2.
The research on aerodynamic characteristics of wrap-around fin and wing-body combination was carried out at super high speeds in this dissertation.
本文开展了弧形翼及翼-身组合体在超高速下的空气动力学特性研究。
