Comfrc Data Acquisition Software For The Amrl Low Speed Wind Tunnel PDF Download

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COMFRC

COMFRC
Author: Craig D. Edwards
Publisher:
Total Pages: 37
Release: 2001
Genre: Information storage and retrieval systems
ISBN:

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The data acquisition system in the Low Speed Wind Tunnel (LSWT) at the Aeronautical and Maritime Research Laboratory (AMRL) was upgraded recently. A new UNIX based host computer provides a C and X/Motif software development environment. COMFRC is the primary software responsible for the data acquisition, data reduction and storage of data in the LSWT. The operator can follow a test schedule and take data accordingly from a single graphical user interface. The operator can follow a test schedule and take data accordingly from a single graphical user interface. Data and results are displayed in real time during the acquisition process. This document provides details of the new data acquisition system and its operation. The procedures required to configure and carry out an entire wind tunnel test using COMFRC and a suite of associated software packages are described in detail.


COMFRC: Data Acquisition Software for the AMRL Low Speed Wind Tunnel

COMFRC: Data Acquisition Software for the AMRL Low Speed Wind Tunnel
Author:
Publisher:
Total Pages: 50
Release: 2001
Genre:
ISBN:

Download COMFRC: Data Acquisition Software for the AMRL Low Speed Wind Tunnel Book in PDF, ePub and Kindle

The data acquisition system in the Low Speed Wind Tunnel (LSWT) at the Aeronautical and Maritime Research Laboratory (AMRL) was upgraded recently. A new UNIX based host computer provides a C and X/Motif software development environment. COMFRC is the primary software responsible for the data acquisition, data reduction and storage of data in the LSWT. The operator can follow a test schedule and take data accordingly from a single graphical user interface. Data and results are displayed in real time during the acquisition process. This document provides details of the new data acquisition system and its operation. The procedures required to configure and carry out an entire wind tunnel test using COMFRC and a suite of associated software packages are described in detail.


Application of a PC Based, Real-Time, Data-Aquisition System in Rotorcraft Wind-Tunnel Testing

Application of a PC Based, Real-Time, Data-Aquisition System in Rotorcraft Wind-Tunnel Testing
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
Total Pages: 38
Release: 2018-08-16
Genre:
ISBN: 9781725147508

Download Application of a PC Based, Real-Time, Data-Aquisition System in Rotorcraft Wind-Tunnel Testing Book in PDF, ePub and Kindle

Data has been acquired for a rotocraft test in the NASA Langley Transonic Dynamics Tunnel using a desktop data acquisition system. The system, which consists of an IBM Personal Computer AT (PC-AT) and an Omega Engineering OM-900 Stand-Alone Interface System, is well suited for acquiring high speed data on a limited number of channels. The data acquisition system and the interrupt driven software which provides the capability for near real-time cyclic data acquisition as well as data storage and display are described. Wilbur, Matthew L. Langley Research Center NASA-TM-4119, L-16565, NAS 1.15:4119, AVSCOM-TM-89-B-003, AD-A213083 RTOP 505-63-51-03...


Development of a Force and Airspeed Data Acquisition System for the Embry-Riddle Aeronautical University 30x40 In. Subsonic Wind Tunnel

Development of a Force and Airspeed Data Acquisition System for the Embry-Riddle Aeronautical University 30x40 In. Subsonic Wind Tunnel
Author: Hong Foo Toon
Publisher:
Total Pages: 174
Release: 2003
Genre: Automatic data collection systems
ISBN:

Download Development of a Force and Airspeed Data Acquisition System for the Embry-Riddle Aeronautical University 30x40 In. Subsonic Wind Tunnel Book in PDF, ePub and Kindle

"This thesis will emphasize on the new data acquisition program written in the LabVIEW environment in 2000. [snip] The system described in this thesis is capable of reading values from various instruments and reducing those data to yield aerodynamic loads, coefficients, temperatures and air velocities."--Leaf v.