Design And Calibration Of The Mixing Layer And Wind Tunnel
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Design And Calibration Of The Mixing Layer And Wind Tunnel
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07
Design And Calibration Of The Mixing Layer And Wind Tunnel written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07 with categories.
A detailed account of the design, assembly and calibration of a wind tunnel specifically designed for free-shear layer research is contained. The construction of this new facility was motivated by a strong interest in the study of plane mixing layers with varying initial and operating conditions. The Mixing Layer Wind tunnel is located in the Fluid Mechanics Laboratory at NASA Ames Research Center. The tunnel consists of two separate legs which are driven independently by centrifugal blowers connected to variable speed motors. The blower/motor combinations are sized such that one is smaller than the other, giving maximum flow speeds of about 20 and 40 m/s, respectively. The blower speeds can either be set manually or via the Microvax II computer. The two streams are allowed to merge in the test section at the sharp trailing edge of a slowly tapering splitter plate. The test section is 36 cm in the cross-stream direction, 91 cm in the spanwise direction and 366 cm in length. One test section side-wall is slotted for probe access and adjustable so that the streamwise pressure gradient may be controlled. The wind tunnel is also equipped with a computer controlled, three-dimensional traversing system which is used to investigate the flow fields with pressure and hot-wire instrumentation. The wind tunnel calibration results show that the mean flow in the test section is uniform to within plus or minus 0.25 pct and the flow angularity is less than 0.25 deg. The total streamwise free-stream turbulence intensity level is approximately 0.15 pct. Currently the wind tunnel is being used in experiments designed to study the three-dimensional structure of plane mixing layers and wakes. Bell, James H. and Mehta, Rabindra D. Unspecified Center NCC2-55...
Design And Calibration Of The Mixing Layer And Wind Tunnel
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Author : Joint Institute for Aeronautics and Acoustics
language : en
Publisher:
Release Date : 1989
Design And Calibration Of The Mixing Layer And Wind Tunnel written by Joint Institute for Aeronautics and Acoustics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with categories.
Design Construction And Calibration Of A Boundary Layer Research Wind Tunnel
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Author : Omeed Alahverdizadeh
language : en
Publisher:
Release Date : 1985
Design Construction And Calibration Of A Boundary Layer Research Wind Tunnel written by Omeed Alahverdizadeh and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1985 with categories.
Design And Calibration Of An Arc Heated Hypersonic Low Density Wind Tunnel
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Author : Ruth N. Weitmann
language : en
Publisher:
Release Date : 1962
Design And Calibration Of An Arc Heated Hypersonic Low Density Wind Tunnel written by Ruth N. Weitmann and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Chemistry, Physical and theoretical categories.
Design Construction And Testing Of A Two Stream Mixing Layer Wind Tunnel Facility
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Author : Mohammed Naveed Anwer
language : en
Publisher:
Release Date : 1985
Design Construction And Testing Of A Two Stream Mixing Layer Wind Tunnel Facility written by Mohammed Naveed Anwer and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1985 with Wind tunnels categories.
Design And Calibration Of A Wind Tunnel
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Author : Peter Otton Tauson
language : en
Publisher:
Release Date : 1936
Design And Calibration Of A Wind Tunnel written by Peter Otton Tauson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1936 with Aerodynamics categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1995
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Aeronautics categories.
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Wind Tunnel Calibration Techniques
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Author : Alan Pope
language : en
Publisher:
Release Date : 1961
Wind Tunnel Calibration Techniques written by Alan Pope and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Wind tunnels categories.
Air-flow measuring instruments, their use, and the manner of working up and presenting the data obtained when calibrating low-speed, nearsonic, transonic, supersonic, and hypersonic wind tunnels are discussed. (Author).
Calibration Of Boundary Layer Wind Tunnel
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Author : Edward L. Dashefsky
language : en
Publisher:
Release Date : 1936
Calibration Of Boundary Layer Wind Tunnel written by Edward L. Dashefsky and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1936 with categories.
Design And Calibration Of An Arc Heated Hypersonic Low Density Wind Tunnel
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Author : Ruth N. Weltmann
language : en
Publisher:
Release Date : 1962
Design And Calibration Of An Arc Heated Hypersonic Low Density Wind Tunnel written by Ruth N. Weltmann and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with categories.
