User's Manual for the Langley Research Center 14- by 22- Foot Subsonic Tunnel Static Data Acquisition System PDF Download
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Author:
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Category :
Languages : en
Pages : 112
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Author:
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ISBN:
Category :
Languages : en
Pages : 112
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Author: P. Frank Quinto
Publisher:
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Category : Aerodynamics
Languages : en
Pages : 68
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Category : Aeronautics
Languages : en
Pages : 704
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Category : Government publications
Languages : en
Pages : 1064
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Author:
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Category : Government publications
Languages : en
Pages :
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Category : Government publications
Languages : en
Pages : 1374
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Category :
Languages : en
Pages : 392
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Author:
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Category : Aeronautics
Languages : en
Pages : 312
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Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723478475
Category :
Languages : en
Pages : 110
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The Static Data Acquisition System (SDAS) components primarily responsible for acquiring data at the 14- by 22-Foot Subsonic Tunnel are the NEFF 620/600 Data Acquisition Unit (DAU) and the PSI 780B electronically scanned pressure (ESP) measurement system. A 9250 Modcomp computer is used to process the signal, to do all aerodynamic calculation, and to control the output of data. All of the tasks required to support a wind tunnel investigation are menu driven. The purpose of this report is to acquaint users of this system with the wide range of capabilities that exist with the available hardware and software and provide them with the proper procedures to follow when setting up or running individual tests. Orie, Nettie M. and Quinto, P. Frank Langley Research Center AERODYNAMICS; DATA ACQUISITION; SUBSONIC WIND TUNNELS; USER MANUALS (COMPUTER PROGRAMS); WIND TUNNEL TESTS; COMPUTER PROGRAMS; COMPUTERS; CONTROL SYSTEMS DESIGN; PRESSURE MEASUREMENT...
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Category : Science
Languages : en
Pages : 1142
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