Langley 14- by 22-foot Subsonic Tunnel Test Engineer's Data Acquisition and Reduction Manual

Langley 14- by 22-foot Subsonic Tunnel Test Engineer's Data Acquisition and Reduction Manual PDF Author: P. Frank Quinto
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 68

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Langley 14- by 22-foot Subsonic Tunnel Test Engineer's Data Acquisition and Reduction Manual

Langley 14- by 22-foot Subsonic Tunnel Test Engineer's Data Acquisition and Reduction Manual PDF Author: P. Frank Quinto
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 68

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 836

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1994

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1450

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 182

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User's Manual for the Langley Research Center 14- by 22- Foot Subsonic Tunnel Static Data Acquisition System

User's Manual for the Langley Research Center 14- by 22- Foot Subsonic Tunnel Static Data Acquisition System PDF Author:
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ISBN:
Category :
Languages : en
Pages : 112

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Langley 14- By 22-Foot Subsonic Tunnel Test Engineer's Data Acquisition and Reduction Manual

Langley 14- By 22-Foot Subsonic Tunnel Test Engineer's Data Acquisition and Reduction Manual PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722611507
Category :
Languages : en
Pages : 64

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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...

Aeronautical Enginnering: A Cumulative Index to a Continuing Bibliography (supplement 312)

Aeronautical Enginnering: A Cumulative Index to a Continuing Bibliography (supplement 312) PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 392

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NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 88

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Government Reports Annual Index

Government Reports Annual Index PDF Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1374

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