An Experimental Investigation of Structure, Mixing and Combustion in Compressible Turbulent Shear Layers [microform]

An Experimental Investigation of Structure, Mixing and Combustion in Compressible Turbulent Shear Layers [microform]
Author: Hall, Jeffery L
Publisher: Ann Arbor, Mich. : University Microfilms International
Total Pages: 139
Release: 1991
Genre: Electronic dissertations
ISBN:

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Two-dimensional, compressible, turbulent shear layers are studied in a new wind tunnel facility. Both reacting and non-reacting flows are investigated, with one free stream velocity supersonic and the other subsonic. The combustion experiments are based on use of low concentrations of hydrogen, nitric oxide and fluorine gases. Side-view Schlieren photographs of these reacting and non-reacting flows appear devoid of the 2-D, large scale structures seen in incompressible flow. Comparison with all-subsonic flows produced in the same facility suggests that this lack of two-dimensional structure is due to the presence of the supersonic high-speed free stream velocity. Travelling shock and expansion waves are observed in the high compressibility flows, evidently created by turbulent structures convecting at supersonic velocities. Such waves are seen only in the low-speed fluid, with apparent convection velocities much higher than those predicted on the basis of isentropic pressure-matching arguments. The measured shear layer growth rates agree with previous results by other experiments, except for a few cases at low compressibility and low density ratio. The fast chemistry regime is attained in some of the high compressibility flows tested. 'Flip' experiments conducted in this regime indicated that the volume fraction of mixed fluid in the layer is substantially reduced as compared to previous incompressible results. These same flip experiments also reveal that compressibility significantly alters the entrainment ratio.

An Experimental Investigation of Structure, Mixing and Combustion in Compressible Turbulent Shear Layers

An Experimental Investigation of Structure, Mixing and Combustion in Compressible Turbulent Shear Layers
Author: Jeffery Lawrence Hall
Publisher:
Total Pages: 139
Release: 1991
Genre: Electronic dissertations
ISBN:

Download An Experimental Investigation of Structure, Mixing and Combustion in Compressible Turbulent Shear Layers Book in PDF, Epub and Kindle

Two-dimensional, compressible, turbulent shear layers are studied in a new wind tunnel facility. Both reacting and non-reacting flows are investigated, with one free stream velocity supersonic and the other subsonic. The combustion experiments are based on use of low concentrations of hydrogen, nitric oxide and fluorine gases. Side-view Schlieren photographs of these reacting and non-reacting flows appear devoid of the 2-D, large scale structures seen in incompressible flow. Comparison with all-subsonic flows produced in the same facility suggests that this lack of two-dimensional structure is due to the presence of the supersonic high-speed free stream velocity. Travelling shock and expansion waves are observed in the high compressibility flows, evidently created by turbulent structures convecting at supersonic velocities. Such waves are seen only in the low-speed fluid, with apparent convection velocities much higher than those predicted on the basis of isentropic pressure-matching arguments. The measured shear layer growth rates agree with previous results by other experiments, except for a few cases at low compressibility and low density ratio. The fast chemistry regime is attained in some of the high compressibility flows tested. 'Flip' experiments conducted in this regime indicated that the volume fraction of mixed fluid in the layer is substantially reduced as compared to previous incompressible results. These same flip experiments also reveal that compressibility significantly alters the entrainment ratio.

An Experimental Investigation of Organized Structure and Mixing in Compressible Turbulent Free Shear Layers

An Experimental Investigation of Organized Structure and Mixing in Compressible Turbulent Free Shear Layers
Author: Nathan Lee Messersmith
Publisher:
Total Pages: 474
Release: 1992
Genre:
ISBN:

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The large scale structure and scalar transport characteristics of compressible turbulent mixing layers have been experimentally investigated at various levels of compressibility in order to study the fundamental effects of compressibility on the nature of the mixing layer. Nonintrusive optical diagnostic techniques were employed to image the large structures. Both Mie scattering from condensed ethanol droplets and laser-induced fluorescence from seeded nitric oxide were used. The LIF experiments were utilized to avoid potential particle dynamics effects associated with the Mie scattering experiments. Sizeable ensembles of digital images were collected for a variety of seeding styles, image planes and at three distinct flow conditions. Analysis of the samples provided mean and standard deviation profiles, two-dimensional spatial covariance fields and passive scalar probability density functions. In the transverse image plane, the dimensionless structure size and eccentricity increased, while the angular orientation of the structures with respect to the streamwise flow direction decreased, as the relative Mach number increased. Oblique views revealed significant three-dimensionality, and the structures imaged in this view also increased in dimensionless size with compressibility. Very little difference in the total probabilities of finding mixed fluid within the shear layer was found for flows with relative Mach numbers of 0.63 and 1.49. A relative Mach number 0.98 flow, however, demonstrated substantially lower mixed fluid probabilities, concomitant with a very high peak standard deviation. Instability mode interactions may be the cause of the disturbed nature of the mixing layer at this condition. The results from the Mie scattering and laser-induced fluorescence experiments for similar shear layer conditions were very comparable.

Turbulent Shear Layers in Supersonic Flow

Turbulent Shear Layers in Supersonic Flow
Author: Alexander J. Smits
Publisher: Springer Science & Business Media
Total Pages: 418
Release: 2006-05-11
Genre: Science
ISBN: 0387263055

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A good understanding of turbulent compressible flows is essential to the design and operation of high-speed vehicles. Such flows occur, for example, in the external flow over the surfaces of supersonic aircraft, and in the internal flow through the engines. Our ability to predict the aerodynamic lift, drag, propulsion and maneuverability of high-speed vehicles is crucially dependent on our knowledge of turbulent shear layers, and our understanding of their behavior in the presence of shock waves and regions of changing pressure. Turbulent Shear Layers in Supersonic Flow provides a comprehensive introduction to the field, and helps provide a basis for future work in this area. Wherever possible we use the available experimental work, and the results from numerical simulations to illustrate and develop a physical understanding of turbulent compressible flows.

High-Speed Flight Propulsion Systems

High-Speed Flight Propulsion Systems
Author: S. N. B. Murthy
Publisher: AIAA
Total Pages: 558
Release: 1991
Genre: Aerodynamics, Hypersonic
ISBN: 9781600863912

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Annotation Leading researchers provide a cohesive treatment of the complex issues in high-speed propulsion, as well as introductions to the current capabilities for addressing several fundamental aspects of high-speed vehicle propulsion development. Includes more than 380 references, 290 figures and tables, and 185 equations.