Langley 14- by 22-foot Subsonic Tunnel Test Engineer's Data Acquisition and Reduction Manual PDF Download
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Author: P. Frank Quinto
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 68
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Book Description
Author: P. Frank Quinto
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 68
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Book Description
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722611507
Category :
Languages : en
Pages : 64
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Book Description
The Langley 14- by 22-Foot Subsonic Tunnel is used to test a large variety of aircraft and nonaircraft models. To support these investigations, a data acquisition system has been developed that has both static and dynamic capabilities. The static data acquisition and reduction system is described; the hardware and software of this system are explained. The theory and equations used to reduce the data obtained in the wind tunnel are presented; the computer code is not included. Quinto, P. Frank and Orie, Nettie M. Langley Research Center...
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 836
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Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1994
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1450
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 182
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Author:
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ISBN:
Category :
Languages : en
Pages : 112
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Author:
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ISBN:
Category :
Languages : en
Pages : 392
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Author:
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ISBN:
Category : Science
Languages : en
Pages : 88
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1374
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