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Description: sf-supersonic.zip
a ftp search engine(HIT)-sf - supersonic.zip a ftp search engine (HI T)
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Size: 3424686 |
Author: cutepig |
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Description: 项目名称:超声波测距接收部分程序
功 能: 晶振采用12M，引脚定义：P0.1(SDA),P0.2(SCL),P3.2(即INT0,红外输入),P3.3(即INT1,超声波输入)
硬件环境: 自制单片机实验板，
软件环境: Windows操作系统
使用软件：伟福 V3.20,
Easy 51Pro v2.0
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Size: 2881 |
Author: liangweiyuan |
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Description: sf-supersonic.zip
a ftp search engine(HIT)-sf- supersonic.zip a ftp search engine (HI T)
Platform: |
Size: 3424256 |
Author: |
Hits:
Description: 项目名称:超声波测距接收部分程序
功 能: 晶振采用12M，引脚定义：P0.1(SDA),P0.2(SCL),P3.2(即INT0,红外输入),P3.3(即INT1,超声波输入)
硬件环境: 自制单片机实验板，
软件环境: Windows操作系统
使用软件：伟福 V3.20,
Easy 51Pro v2.0-Project Name: Ultrasonic Distance Measurement receive some program features: crystal using 12M, pin definition: P0.1 (SDA), P0.2 (SCL), P3.2 (that is, INT0, infrared input), P3.3 ( that is, INT1, ultrasonic input) Hardware Environment: self-made single-chip board, software environment: Windows operating system using the software: Wei Fu-V3.20, Easy 51Pro v2.0
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Size: 3072 |
Author: liangweiyuan |
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Description: 所以请不要将文件放在这两个目录下超声速流二维守恒-Therefore, please do not file on these two directories under the two-dimensional supersonic flow conservation
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Size: 449536 |
Author: huangyue |
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Description: 2维超音速流的Prandtl-Meyer膨胀破的fortran程序-2-dimensional supersonic flow of the Prandtl-Meyer expansion of breaking the fortran program
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Size: 231424 |
Author: 张杰 |
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Description: 这是彩色B超管理软件，人员管理部分基本未完成，图象采集部份还没有完成，后来因为各种原因没机会再完善了。-This is the color B-management software, personnel management unfinished part of the capital, part of the image acquisition is not yet complete, and later due to various reasons, no chance to improve.
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Size: 1465344 |
Author: 李达 |
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Description: 一个使用mcu制作的频率回扫超声波程序，mcu采用c51/stc等系列-The mcu production ultrasonic frequency flyback program
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Size: 1024 |
Author: pzhihui |
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Description: 模拟一维拉法尔喷管的跨音速流动，出口条件为超音速，参见空气动力学教材-subsonic-supersonic flow in one dimensional laval nozzle,the outflow velocity is supersonic
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Size: 2048 |
Author: 长春 |
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Description: 超声速光学头罩流场的PIV研究，应用在超声速光学头罩流场的PIV研究-Supersonic flow field of optical PIV hood research, application in the supersonic flow field of optical PIV study of Hood
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Size: 2097152 |
Author: yongge |
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Description: theoratical stability derivatives for a symmetrically tapered wing at low supersonic speed
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Size: 862208 |
Author: asad |
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Description: Modified runge kutta integration for supersonic vehicle
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Size: 1024 |
Author: niteen |
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Description: 计算二维圆钝体超声速流动的一个Fortran程序-Calculated two-dimensional blunt body in supersonic flow of a Fortran program
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Size: 7168 |
Author: 吴方 |
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Description: 单片机的声音与超声波检测应用程序，对初学者非常有用-programs of 80c51 for audio and supersonic application
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Size: 3072 |
Author: zbchen69 |
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Description: 利用显示MacCormack时间步计算二维超声速绕平板流，对于研究计算流体力学有很大帮助-A Fortran program of two-dimensional Navier-Stokes equations for the supersonic flow over a flat plate based on MacCormack s explicit time-marching technique.
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Size: 709632 |
Author: wangxing |
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Description: computer program for the calculation of steady three dimensional adiabatic flows in supersonic rocket engine nozzles. The fluid is assumed to be an inviscid perfect gas and the flow is assumed to be shock free. The governing equations for this flow model consist of the continuity equation, the momentum equations, and the speed of sound equation. The steady three dimensional supersonic flows is computed using a pentahedral bicharacteristic method. An inverse marching method based on the network of wavelines and the pathline is employed. The spline surface fit is used in the iteration procedure to evaluate the location of the unknown point in the new reference plane and its flow properties-computer program for the calculation of steady three dimensional adiabatic flows in supersonic rocket engine nozzles. The fluid is assumed to be an inviscid perfect gas and the flow is assumed to be shock free. The governing equations for this flow model consist of the continuity equation, the momentum equations, and the speed of sound equation. The steady three dimensional supersonic flows is computed using a pentahedral bicharacteristic method. An inverse marching method based on the network of wavelines and the pathline is employed. The spline surface fit is used in the iteration procedure to evaluate the location of the unknown point in the new reference plane and its flow properties
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Size: 5341184 |
Author: AALI |
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Description: supersonic wave LCD1602 desinged for little smart car
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Size: 28672 |
Author: 费德勒 |
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Description: 这是一个c51的代码，可以实现超声波测距的功能，谢谢大家惠顾。-this is a program which could measure distance with supersonic distance measurement.
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Size: 103424 |
Author: yyy |
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Description: 随着计算机应用的普及，对便携式输入设备的要求也越来越高。人们希望能随时随地用电子设备记录下原始的书写内容。传统的基于传感材料的手写笔系统需要特殊的书写材料，使它的应用范围受到限制。超声波相对与电磁波速度要小得多，其传播的时间较容易检测，将其应用于电子笔系统中，可以使输入设备更加便捷，笔迹跟踪准确。-supersonic electronic pen design by TMS320VC5509A
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Size: 106496 |
Author: Andy |
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Description: 计算流体力学基础及应用第9章，非本人编写。超音速平板绕流数值计算程序(Computational fluid dynamincs. JohnD. Anderson Chapter9_Version_3 supersonic flow over flat plate code)
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Size: 59392 |
Author: wdbwf |
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