Aiaa journal文章索引

期刊名：Aiaa journal

缩写：AIAA J

ISSN：0001-1452

e-ISSN：1533-385X

IF/分区：3.2/Q1

共收录本刊相关文章索引3962条

Hybrid Explicit-Implicit, Unconditionally Stable Scheme for Unsteady Compressible Flows [0.03%] 用于非定常可压缩流的混合显式-隐式、无条件稳定格式

Men'Shov, Igor; Nakamura, Yoshiaki Men'Shov

AIAA Journal. 2004;42(3):551-559. DOI:10.2514/1.9109 2004

Microfabricated Shear Stress Sensors, Part 2: Testing and Calibration [0.03%] 微加工剪切应力传感器，第2部分：测试与校准

Hyman, Dan; Pan, Tao; Reshotko et al. Hyman et al.

AIAA Journal. 1999;37(1):73-78. DOI:10.2514/2.666 1999

Cracking-Induced Mistuning in Bladed Disks [0.03%] 叶盘中由裂纹引起的失谐

Hou, Jian F. Hou

AIAA Journal. 2006;44(11):2542-2546. DOI:10.2514/1.21494 2006

A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows. [0.03%] 一种用于计算亚音速流中振荡表面上升力分布的双层格子方法。

AIAA Journal. 1969;7(2):279-285. DOI:10.2514/3.5086 1969

Accelerated convergence of Euler solutions using time inclining [0.03%] 利用时间倾斜加速欧拉解的收敛性

DANNENHOFFER, , III et al. DANNENHOFFER et al.

AIAA Journal. 1990;28(8):1457-1463. DOI:10.2514/3.25238 1990

Flow Separation Control by Plasma Actuator with Nanosecond Pulsed-Periodic Discharge [0.03%] 基于纳秒脉冲周期放电的等离子体作动器的流动分离控制

Roupassov, D. V.; Nikipelov, A. A.; Nudnova et al. Roupassov et al.

AIAA Journal. 2009;47(1):168-185. DOI:10.2514/1.38113 2009

Finite-Core Vortex Array Model of the Wake of a Periodically Pitching Airfoil [0.03%] 周期性俯仰翼型尾流的有限核心涡旋阵列模型

Naguib, A. M.; Vitek, J.; Koochesfahani et al. Naguib et al.

AIAA Journal. 2011;49(7):1542-1550. DOI:10.2514/1.J050881 2011

Improved theory for contact indentation of sandwich panels [0.03%] 夹层板接触压痕的改进理论

AIAA Journal. 1996;34(6):1238-1244. DOI:10.2514/3.13218 1996

Master Plan for Prediction of Vehicle Interior Noise [0.03%] 车辆内部噪声预测总体规划

AIAA Journal. 1980;18(4):353-366. DOI:10.2514/3.50767 1980

Effects of Pressure Gradients on Turbulent Boundary Layer Wave Number Frequency Spectra [0.03%] 压力梯度对湍流边界层波数频率谱的影响

Cipolla, K.; Keith, W. Cipolla

AIAA Journal. 2000;38(10):1832-1836. DOI:10.2514/2.864 2000