Flow Generation Properties of Five Transonic Wind Tunnel Test Section Wall Configurations PDF Download
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Author: R. L. Parker (Jr.)
Publisher:
ISBN:
Category : Porosity
Languages : en
Pages : 52
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Book Description
Author: R. L. Parker (Jr.)
Publisher:
ISBN:
Category : Porosity
Languages : en
Pages : 52
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Book Description
Author: R. L Parker (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
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Book Description
Tests were conducted in the Aerodynamic Wind Tunnel (1T) of the Propulsion Wind Tunnel Facility to determine the tunnel calibration and centerline Mach number distribution for five transonic wall configurations. Data were also obtained with a cone-cylinder model to determine the effects of model blockage on the free-stream Mach number development in the test section. During the test, the Mach number was varied from 0.6 to 1.3. The wall porosity was varied to obtain data at representative values for each wall configuration. This report presents the test results and provides data to guide the operation of Tunnel 1T with the five transonic wall configurations. (Author).
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
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Author: B. H. Goethert
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 420
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Book Description
Numerous aspects of transonic aerodynamics include wall interference corrections in conventional wind tunnels, subsonic flow in a variety of wind tunnels, and test results from transonic wind tunnels. 1961 edition.
Author: N. Sam Dougherty (Jr.)
Publisher:
ISBN:
Category : Resonance
Languages : en
Pages : 44
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Author: George M. Stokes
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 60
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Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 882
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Author: J. L. Jacocks
Publisher:
ISBN:
Category :
Languages : en
Pages : 49
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Book Description
An experimental investigation was conducted to record the acoustic and aerodynamic performance of several slotted walls with transverse baffles in the slots for transonic test sections. Primary configuration variables were the baffle angle inclination relative to the airstream and a wire mesh screen on the airside wall surface. At all baffle angles, the addition of the screen overlay decreased the acoustic noise level and improved the flow generation and supersonic wave cancellation properties of the wall but increased the subsonic wall interference effects. (Author).
Author: T. D. Reed
Publisher:
ISBN:
Category : Calibration
Languages : en
Pages : 292
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 852
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