Nasa Lewis 9 By 15 Foot Low Speed Wind Tunnel User Manual

Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722655570
Total Pages : 52 pages
Book Rating : 4.77/5 ( download)

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Download or read book NASA Lewis 9- By 15-Foot Low-Speed Wind Tunnel User Manual written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-10 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: This manual describes the 9- by 15-Foot Low-Speed Wind Tunnel at the Lewis Research Center and provides information for users who wish to conduct experiments in this atmospheric facility. Tunnel variables such as pressures, temperatures, available tests section area, and Mach number ranges (0.05 to 0.20) are discussed. In addition, general support systems such as air systems, hydraulic system, hydrogen system, laser system, flow visualization system, and model support systems are described. Instrumentation and data processing and acquisition systems are also discussed. Soeder, Ronald H. Glenn Research Center...

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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.58/5 ( download)

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Download or read book NASA Lewis 9- by 15-foot Low-speed Wind Tunnel User Manual written by and published by . This book was released on 1993 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Milo D. Dahl
Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.64/5 ( download)

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Download or read book Acoustical Evaluation of the NASA Lewis 9 by 15 Foot Low Speed Wind Tunnel written by Milo D. Dahl and published by . This book was released on 1992 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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ISBN 13 :
Total Pages : 190 pages
Book Rating : 4.91/5 ( download)

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Download or read book Calibration of the NASA Lewis Research Center 9- by 15-Foot Low Speed Wind Tunnel (1994 Test) written by and published by . This book was released on 1997 with total page 190 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.78/5 ( download)

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Download or read book User Manual for NASA Lewis 10 by 10 Foot Supersonic Wind Tunnel written by and published by . This book was released on 1995 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
ISBN 13 : 9781730909931
Total Pages : 80 pages
Book Rating : 4.30/5 ( download)

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Download or read book Flowfield Measurements in the NASA Lewis Research Center 9- By 15-Foot Low-Speed Wind Tunnel written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-11-06 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: ational Aeronautics and Space Administration

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ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.19/5 ( download)

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Download or read book NASA Lewis Icing Research Tunnel User Manual written by and published by . This book was released on 1996 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: This manual describes the Icing Research Tunnel (IRT) at the NASA Lewis Research Center and provides information for users who wish to conduct experiments in this facility. The capabilities of the tunnel test section, main drive system, speed control system, and spray bars are described. Tunnel performance maps of liquid water content as a function of median volume droplet size is presented for two types of spray nozzles at test-section velocities ranging from 86.8 to 303.9 kn (100 to 350 mph). The facility support systems, which include heated air systems, steam and service air systems, an altitude exhaust system, a force balance system, and the model electrical power system, are described. Also discussed are facility instrumentation capabilities for temperature and pressure measurements and model attitude simulation. In addition, photographic documentation and flow visualization techniques are explained, and pretest meeting formats and schedules are outlined. Tunnel-user responsibilities, personnel safety requirements, and types of test agreements are explained. The IRT is a closed-return atmospheric tunnel with a test section that is 6 ft high, 9 ft wide, and 20 ft long. It is equipped to support testing at airspeeds up to 303.9 kn (350 mph) with a 5.0-percent blockage model in the test section in a temperature and water-droplet environment that simulates natural icing conditions.

Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
ISBN 13 : 9781730733956
Total Pages : 56 pages
Book Rating : 4.56/5 ( download)

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Download or read book User Manual for NASA Lewis 10 by 10 Foot Supersonic Wind Tunnel. Revised written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-11 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: This manual describes the 10- by 10-Foot Supersonic Wind Tunnel at the NASA Lewis Research Center and provides information for users who wish to conduct experiments in this facility. Tunnel performance operating envelopes of altitude, dynamic pressure, Reynolds number, total pressure, and total temperature as a function of test section Mach number are presented. Operating envelopes are shown for both the aerodynamic (closed) cycle and the propulsion (open) cycle. The tunnel test section Mach number range is 2.0 to 3.5. General support systems, such as air systems, hydraulic system, hydrogen system, fuel system, and Schlieren system, are described. Instrumentation and data processing and acquisition systems are also described. Pretest meeting formats and schedules are outlined. Tunnel user responsibility and personnel safety are also discussed. Soeder, Ronald H. Glenn Research Center...

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ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.07/5 ( download)

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Download or read book NASA Lewis 8- by 6-foot Supersonic Wind Tunnel User Manual written by and published by . This book was released on 1993 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : National Aeronautics and Space Adm Nasa
Publisher :
ISBN 13 : 9781729382097
Total Pages : 58 pages
Book Rating : 4.96/5 ( download)

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Download or read book NASA Lewis 8- By 6-Foot Supersonic Wind Tunnel User Manual written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-10-29 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: The 8- by 6-Foot Supersonic Wind Tunnel (SWT) at Lewis Research Center is available for use by qualified researchers. This manual contains tunnel performance maps which show the range of total temperature, total pressure, static pressure, dynamic pressure, altitude, Reynolds number, and mass flow as a function of test section Mach number. These maps are applicable for both the aerodynamic and propulsion cycle. The 8- by 6-Foot Supersonic Wind Tunnel is an atmospheric facility with a test section Mach number range from 0.36 to 2.0. General support systems (air systems, hydraulic system, hydrogen system, infrared system, laser system, laser sheet system, and schlieren system are also described as are instrumentation and data processing and acquisition systems. Pretest meeting formats are outlined. Tunnel user responsibility and personal safety requirements are also stated. Soeder, Ronald H. Glenn Research Center...