机译:吸入和脉冲吹流控制应用于轴对称体
NASA Ames Research Center, Moffett Field, California 94035,Aeroflightdynamics Directorate, U.S. Army Aviation Development Directorate - AFDD Aviation & Missile Research, Development & Engineering Center Research, Development and Engineering Command, Mail Stop 215-1;
Science and Technology Corporation, Moffett Field, California 94035,Aeroflightdynamics Directorate, U.S. Army Aviation Development Directorate - AFDD Aviation & Missile Research, Development & Engineering Center Research, Development and Engineering Command, Mail Stop 215-1;
Rafael Ltd., 31021 Haifa, Israel,Computational Fluid Dynamics, Aeronautical Systems, Mail Stop 39870;
Tel Aviv University, 69978 Tel Aviv, Israel,School of Mechanical Engineering, Wolfson M.E. Bldg., Rm. 217, Levanon Street;
Tel Aviv University, 69978 Tel Aviv, Israel,School of Mechanical Engineering, Wolfson M.E. Bldg., Rm. 217, Levanon Street;
机译:利用中心体表面的吸力通过涡流细胞中的流动增强来控制流过厚翼型的湍流
机译:用于流量控制的脉冲吹塑系统建模
机译:具有可变特性和吸力的圆柱体上轴对称停滞流中微极性流体的流动和传热(数值研究)
机译:流量控制对运动的轴对称钝体产生的非稳态气动载荷
机译:平面和轴对称非定常流经振动体的数值模拟。
机译:通过不对称流量控制提高高压比涡轮增压器离心压缩机的稳定性-第一部分:离心压缩机中的非轴对称流量
机译:具有多孔抽吸条的轴对称体流动的稳定性
机译:吸气或吹气二维和轴对称体周围层流和湍流边界层的计算方法