@techreport{oai:jaxa.repo.nii.ac.jp:00043509,
 author = {柳沢, 三憲 and Yanagizawa, Mitsunori},
 month = {Dec},
 note = {A procedure for the numerical solution of steady flow past a wing with fans is descried using a boundary element method in potential flow. The effect of thrust is represented by doublet singularities. The method employs an aerodynamic panel code to simulate the flow of fan jet stream around an aircraft configuration. The configuration of a VTOL transport in achieving a multijet lifting system is composed of lifting fans nested in the wing planform. The aerodynamic forces were calculated with the fundamental shape of FAN IN WING. The result is that there are regions of negative lift behind the position of the lift fan on the wing. The general tendency of how they interact with the wing to produce the aerodynamic forces is understood., 資料番号: NALSP0016013, レポート番号: NAL SP-16},
 title = {境界要素法による推力付翼の空力計算},
 year = {1991}
}