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matrix22
- 求解旋量玻色爱因斯坦凝聚单个涡旋态的mathematics程序，其中遇到的矩阵的本证值和本证矢量-Solving spinor Bose-Einstein condensates singly quantized vortex mathematics program, of which the matrix encountered the card value and this card vector
length-scaleCs
- 求解旋量玻色爱因斯坦凝聚单个涡旋态的mathematics程序，其中矩阵的本征值和本征矢量-Solving spinor Bose-Einstein condensates singly quantized vortex mathematics program, of which the matrix encountered the card value and this card vector
de-Broglie-wave-length
- 求解旋量玻色爱因斯坦凝聚单个涡旋态的mathematics程序，其中计算原子德布罗意波长的程序。-Solving spinor Bose-Einstein condensates singly quantized vortex mathematics program, which calculated the atomic de Broglie wavelength of the program.
Bose-Hubbard44
- 求解旋量玻色-哈伯德模型的mathematics程序。 -Solving spinor Bose-Einstein condensates singly quantized vortex mathematics program, which calculated the atomic de Broglie wavelength of the program.
VortexBall3
- 用mathematics编写的求解大N近似下球形BEC单个涡旋解的程序。-Written using mathematics to solve big N spherical the BEC a single vortex solution program.
BigNml23
- 用FORTRAN编写的求解大N近似下钠原子球形BEC单个涡旋解的程序。-Written in FORTRAN solving big N sodium atom spherical BEC single vortex solution procedures.
gdth
- Linux driver for ICP vortex GmbH: GDT ISA/EISA/PCI Disk Array Controllers Intel Corporation: Storage RAID Controllers - Linux driver for ICP vortex GmbH: GDT ISA/EISA/PCI Disk Array Controllers Intel Corporation: St
flapping
- 使用非定常涡格法(UVLM)计算一种简单扑翼机的升力。对应文献Time Domain Modeling of Unsteady Aerodynamic Forces on a Flapping Airfoil -Eric Durand（MIT Master thesis）-Unsteady vortex lattice method (UVLM) a simple flapping wing machine lift. Correspo
wogewoge0
- 涡格法求解翼型的气动力，包括阻力 升力 法向力-Vortex lattice method for solving the the aerodynamic airfoil, including resistance lift normal force
au8830
- Aureal Vortex Soundcard driver for Linux.
au88x0_pcm
- Vortex PCM ALSA driver for Linux.
au88x0
- ALSA Linux Device driver for the Aureal Vortex family of soundprocessors.
au88x0_eq
- Aureal Vortex Hardware EQ control/access driver for Linux.
au88x0_core
- Vortex core low level functions driver for Linux.
w12sc3
- W12SC3是美国基于USSAERO程序的超声速机翼设计及分析代码，可用于机翼的整个设计、分析及优化过程。-W12SC3- Supersonic wing design and analysis using source and vortex panel singularity distributions, based on the USSAERO program by Woodward. W12SC3 combines sou
ISO_VOR
- 求解二维平面等熵涡的matlab程序，计算流体力学，MacCormack格式，均匀网格-Solving two-dimensional plane isentropic vortex matlab program, computational fluid dynamics, MacCormack format, uniform grid
T135_export
- 涡格法计算现行气动力的matlab代码，用于飞机机翼概念设计阶段的气动力评估-Tornado is a Vortex Lattice Method for linear aerodynamic wing design applications in conceptual aircraft design or in aeronautical education
vlmd
- 计算低速气动力的涡格法程序，来自NASA，可信度高-This is a vortex lattice aerodynamic program from the low speed aerodynamics group at NASA Langley
chua
- 蔡氏混沌系统产生多涡混沌，用于图像处理,主要进行加密解密-Chua s chaotic system to produce multi vortex chaos, for image processing
isentropic_vortex
- matlab环境下编写的求解等熵涡问题，属于CFD入门级代码-matlab environment prepared isentropic vortex problem solving, is the entry-level CFD code