经典的基于ARM的uboot移植教程

解压后，直接用LabVIEW 8.2 打开即可内容包括1、实现了虚拟信号发生器的仿真显示。在虚拟信号发生器的图形显示窗上观察模拟输出信号的波形，有正弦波、方波、三角波。3、实现了虚拟信号发生器的模拟信号输出。①在设定频率、相位、采样频率、幅值后，输出正弦波、方波、三角波信号，并频率计测量信号频率。②滤波。选择不同的截止频率对输出信号进行滤波。

wasp水质模拟软件中文操作说明书，翻译版本，水科学进展

BCH的matlab实现编译，里面有2个主要程序，编码，译码还有编译结果

A*算法 A star 算法（matlab）版本，可以直接使用，包含路径优化

里面有就是多种数据处理工具，非常便利。 1.文本文件操作 1.1征地部标准坐标导出... 2 1.2征地部标准坐标导入... 6 1.3线封闭... 6 1.4点集转面... 7

创造性MATLAB基于fox-li迭代算法的激光谐振腔自再现模模拟MATLAB基于fox-li迭代算法的激光谐振腔自再现模模拟Numeric a l Solving of Difraction im1gr: I E nation二-211-08-0604-b200.20460808-06-0102002040.60.8X AxisXAxisNumerical Solving of Diffraction integralNumeric a Sol/il: of Diffraction integral-+-N=25SEIN08二D月三0.b0201-08-06-0-02020.4060)801-08-06-04-02002a40608AxisXANumerical Solving of Diffraction integralNumerical Solving of Diffract ion integral三色5AEN=15→N=6.25E41b0.10203040.506070809)0.10.20:040.50.607080.9201994-2009ChinaAcademicJounalElectronicPublishingHouseAllrightsreservedhtto:/www.enki.netNumerical Solving of Diffraction integralNumerical Solving of Diffraction intr"gral10A36δ:=4/72!…+…46=020)2441-D.8-0.6-0.4-0200.2040.68-1-0.80.6-0.4-0.200.20.400.81XAXisX Axis201994-2009ChinaAcademicJOurnalElectronicPublishingHouse.Allrightsreservedhttp://www.cnki.net201994-2009ChinaAcademicJOurnalElectronicPublishingHouse.Allrightsreservedhttp://www.cnki.net

数字语音处理及MATLAB仿真_张雪英编着 中的所有源代码和所需语音文件

计算飞机气动特性的软件的说明书，主要应用于概念设计和初步设计阶段TABLE 2AERODYNAMIC OUTPUT AS A FUNCTION OF /CONFIGURATION AND SPEED REGIME● OUTPUT A∨A| LABLED OUTPUT ONLY FOR CON FIGURATIONS WITH STRAIGHT TAPERED SURFACESA OUTPUT ONLY WITH EXPERIMENTAL DATA INPUCONFIGURATION SPEEDSTATIC AERODYN AMIC CHARACTERISTIC OUTPUTDY NAMIC STABILITY CUTPUREGIMECLSUBSONICBODYTRANSONICSUPERSONICHY PERSONICWINGTRANS0NC口▲|口「口百口SUPERSONIC●{a!口口日口HYPERSONIC口!口D口口HORIZONTALTRANS0NCa|▲▲口口|口白SUPERSONIC·a|口口口·『●|●IY PERSONICVERTICAL TAILSUBSONICOR VENTRALTRANSONIC口FINA sUPERSONIC.「百|口HY PERSONICSUBSONICWING-BODYRANSONC口口口o口SUPERSONIC●d|口HY PERSON百口HORIZONTALTRANS0NIc口口口TAIL- BOOYSUPERSONIC口口0口HY PERSONICSUBSONICVERTICAL TAILTRANSONIC口VENTRAL FIN-2 SUPERSONIC.BODY●●|●|●HYPERSONIC口w|NG-B0D￥△ SUBSONIC■口|口|口|口|a口|aaa0|口aaaaTRANSONICO|口TAILSUPERS0NC口百|百口「口。|口HYPERS0NC口口|口口口口口口SUBSON1C●VERTICAL TAILTRANS0NC▲口VENTRAL FINA SUPERSONIC●●|●●HYPERSONICING BOOYSUBSONICHORIZONTAL口日|a口口a「aa}aTRANSONIC|▲|▲▲▲口A SUPERSONIC O。|。口}口|口口|口VERTICAL TAILVENTRAL FINHYPERS0NC口口c1 THE EFFECTS OF JET POW2PELLER POWER, AND GROUND PROXIMITY MAY BE OBTAINED FOR THESE CONFIGURATIONS IF THE REQUIREDNAMELISTS ARE INPUT, THE EFFECTS OF POWER AND GROUND EFFECTS ARE INCLUDED ONLY IN THE SU!C LONGI TUDIN AL STABILITY RESULTS2 DY NAMIC STABILITY RESULTS ARE THE SAME AS WING-BODY3 TKIN VERTICAL TAIL RESULTS MAY BE OBTAINED FOR THESE CONFIGURATIONS IF THE REQUIRED NAMELIST IS INPUTTHESE EFFECTS ARE INCLUDED ONLY IN THE SUBSONIC LATERAL STABILITY DATAREFER TO DATCOM HANDBOOK FOR METHOD LIMITATIONS IF OUTPUT IS NOT OBTAINED5 AVAILABLE ONLY IN COMBINAT:ON WITH A WING OR TAILCC

【实例简介】Turbulence Modeling for CFD_David C.Wilcox(2006_3rd_E).pdf 

文档为串联谐振电路simulink模型，作为电路入门学习，参数可修改。