Flow Field and Noise Characteristics of a Supersonic Impinging Jet PDF Download
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Author: A. Krothapalli
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Category :
Languages : en
Pages :
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Author: A. Krothapalli
Publisher:
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Category :
Languages : en
Pages :
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Author: Vikas Nataraj Bhargav
Publisher:
ISBN:
Category : Aerospace engineering
Languages : en
Pages : 0
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The impinging jet flowfield observed during take-off and landing of a STOVL aircraft is known to be associated with several adverse effects such as strong acoustic emission, unsteady structural loads, loss of engine efficiency due to hot gas ingestion, thermal stresses on the deck surface, and loss of lift. This flowfield has been well studied from the standpoint of characterizing the induced lift forces and moments caused by fountain flows, unique to such a flowfield. However, in the scenario of two such jets operating in tandem where properties are influenced by jet-jet interaction and coupling, are relatively unknown. Also, there is a lack of understanding of the consequences of difference in the momentum-flux and temperature of the two jets on the flow and acoustic properties. Therefore, the fundamental goal of this study is to systematically assess how different parameters such as momentum-flux and temperature affect the flow and acoustic properties of supersonic dual impinging jets. Thus, the three objectives of this study are: (1) How are the characteristics of supersonic dual impinging jets different from those of a supersonic single impinging jet? (2) What is the effect of relative momentum-flux between the two jets, on the aeroacoustic characteristics of supersonic dual impinging jets? (3) What is the effect of relative temperature, on the aeroacoustic characteristics of supersonic dual impinging jets? To address the first objective, experimental investigation of the flowfield associated with two, under-expanded impinging jets operating at a Nozzle Pressure Ratio (NPR) of 2.65, discharged from identical converging nozzles with an exit diameter of 25.4 mm, is performed. Comparisons with a single impinging jet, operating at the same conditions are provided through shadowgraph flow visualizations, nearfield acoustics, and surface pressure measurements. Fountain flow produced by the interaction of wall jets, a unique feature of dual impinging jets, is found to be relatively strong at short impingement heights and contributed to additional loads on the ground surface. Overall flow unsteadiness in dual jets is less than that in a single jet at conditions involving resonance and the fountain upwash plays an important role in the process. Although the feedback mechanism that drives the resonance in both impinging jet configurations is similar and the corresponding instability mode shapes are retained, there are differences in the strengths of the instability modes between the two configurations. To address the second objective, flowfield is characterized by systematically varying the relative jet momentum-flux between the jets. A converging and converging-diverging (CD) nozzle pair, with identical throat and exit diameters, respectively, is employed during the study. The CD (right) nozzle is held at a fixed over-expanded nozzle pressure ratio (NPR) of 3, and the momentum flux of jet from converging (left) nozzle is varied by changing its expansion ratio (ER). Schlieren flow visualization and ground plane surface pressure measurements indicate that the fountain flow position and strength exhibit a strong dependence on the jet momentum flux and a weak dependence on the impingement height. Further, an increase in momentum of the left jet causes the resonance in the right jet to lose its strength and its influence on the unsteadiness of the left jet, owed to the proximity of the fountain flow to the resonating jet. The presence of fountain upwash is found to alter the symmetry of streamlines, shear layer growth characteristics, and turbulent kinetic energy of the right jet. Under certain conditions, the fountain is close enough to significantly interact with the right jet and change the characteristics of the inner shear layer. Thereby, the processes constituting the feedback mechanism are notably altered and culminates in a weaker resonance. To address the third objective, the flowfield is characterized by systematically varying the relative jet temperature between the jets by increasing the temperature of only one of the jets (right). The NPR of the two jets are held fixed at conditions same as those used for the second objective. Qualitative visualization of the flowfield suggests that the left jet and fountain regions remain nearly unaffected by the right jet temperature. However, a corresponding increase in the jet velocity occurs in the right jet. Both the fountain position and its strength are independent of relative jet temperature and a strong function of the jet momentum flux. The increase in jet temperature also results in additional noise in the nearfield and increased unsteadiness on the impingement surface, although the latter is limited to short impingement heights and the region close to the right jet. At higher temperatures, short impingement heights are found to be more susceptible to resonance, with the chief source of resonance originating in the heated jet. At a fixed impingement height, while the jet instability mode shapes are retained, the corresponding impingement tones in the heated jet experience a systematic increment in frequency with rise in temperature. A detailed study of the velocity field suggest that, for a pair of jets at a given relative jet momentum flux, their fountain upwash could contribute to increased unsteadiness in the region around the nozzle (under-surface of the aircraft) at higher jet temperatures. The present experimental study significantly enhances the understanding of the impinging jet flowfield and its associated impacts on the parent aircraft, noise field and nearby structures. From an engineering standpoint, the results from this study will help inform aerodynamicists and structural engineers about the consequences of multi-jet-impingement configurations in STOVL applications. This is done through a systematic characterization of several parameters, which would provide the design guidelines. The three key findings of this study are: (1) Dual impinging jet flow and acoustic fields are strongly influenced by the fountain flow; (2) Fountain strength and placement relative to the jets, plays an important role in influencing the ground induced adverse effects. This in turn depends on the momentum of the jets; (3) Jet temperature can also worsen these effects, although this is a weaker factor than jet momentum From a scientific stand point, the results from this study provide a high fidelity database for the validation of numerical tools on dual impinging jet configuration. Furthermore, the present study provides the baseline data to help study flow and noise control techniques for dual impinging jets.
Author: Mohammed K. Ibrahim
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author:
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Category : Jet planes
Languages : en
Pages : 194
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Author: William K. Blake
Publisher: Academic Press
ISBN: 0128122897
Category : Science
Languages : en
Pages : 504
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Mechanics of Flow-Induced Sound and Vibration, Volume 1: General Concepts and Elementary Sources, Second Edition, enables readers to fully understand flow-induced vibration and sound, unifying the disciplines of fluid dynamics, structural dynamics, vibration, acoustics, and statistics in order to classify and examine each of the leading sources of vibration and sound induced by various types of fluid motion. Starting with classical theories of aeroacoustics and hydroacoustics, a formalism of integral solutions valid for sources near boundaries is developed and then broadened to address different source types, including jet noise, flow tones, dipole sound from cylinders, and cavitation noise. Step-by-step derivations clearly identify any assumptions made throughout. Each chapter is illustrated with comparisons of leading formulas and measured data. Along with its companion, Mechanics of Flow-Induced Sound and Vibration, Volume 2: Complex Flow-Structure Interactions, the book covers everything an engineer needs to understand flow-induced sound and vibration. This book will be essential reading for postgraduate students, and for engineers and researchers with an interest in aerospace, ships and submarines, offshore structures, construction, and ventilation. Presents every important topic in flow-induced sound and vibration Covers all aspects of the topics addressed, from fundamental theory, to the analytical formulas used in practice Provides the building blocks of computer modeling for flow-induced sound and vibration
Author: Seyyed Saman Salehian
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 536
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"The noise generated by supersonic jet is of primary interest in the high-speed flight. In several flight conditions jet exhaust of the propulsion system interacts with solid surfaces. For example, jet impingement on ground for a rocket lift-off, or interactions influenced by the integration of the engine with the airframe. Such complex applications require consideration of the role of acoustic-surface interactions on the noise generation of the jet and its radiation. Numerical analysis of supersonic jet noise involved in these scenarios is investigated by employing Hybrid Large Eddy Simulation - Unsteady Reynolds Averaged Simulation approach to model turbulence. First, the supersonic impinging jet noise reduction using aqueous injectors is investigated. The technique employed to suppress impingement noise, involves injecting liquid water from the ground surface. The Volume of Fluid model is adopted to simulate the two phase flow. The flow field and acoustic results agree well with the existing experimental data. The possible mechanisms of noise reduction by water injection are investigated. Second, supersonic jet noise reduction by employing the shielding effect of a flat plate parallel to the jet is investigated. The numerical simulations model the shielding effect of the flat plate on the acoustics of supersonic jet, and results agree with the corresponding experimental data. The physical mechanisms involved in the flow-surface interactions are investigated. With understanding these mechanisms, a slightly wavy plate is proposed including theoretical background to determine the parameters needed for the way wall to provide acoustic reduction efficiently. Results show that the proposed wavy shield can effectively reduce both the level and extent of the jet noise source as compared to that of a flat shield."--Abstract.
Author: Henry T. Nagamatsu
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 90
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Author: H. Lou
Publisher:
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Category :
Languages : en
Pages :
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Author:
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Category : Jet planes
Languages : en
Pages : 50
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Author: Kalyan Goparaju
Publisher:
ISBN:
Category : Aerospace engineering
Languages : en
Pages : 174
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Jet noise has been a major source of concern for commercial and military aviation sectors alike. The need to assuage the adverse impact of jet noise on human health has led to increased interest in jet noise source identification and noise level minimization/mitigation. Most previous works on common round supersonic jets have primarily explored the ideal case of simple, perfectly expanded jet configurations. In real world scenarios however, many of these simplifications do not hold. Two such considerations are examined in this work. The first is a simple configuration operating at complex operating conditions, specifically an imperfect expansion i.e. where the jets are operating at off-design conditions. The second concerns a complex configuration at simple conditions: specifically two jets (twin-jets such as those on fighter aircraft) operating in close proximity to each other. In this work, Large Eddy Simulation (LES) based high-fidelity computations are used to understand the dynamics of imperfectly expanded and twin-jets respectively, with the following objectives: 1) Identify the impact of active flow control techniques on the plume dynamics and acoustic characteristics of underexpanded jets, and 2) Investigate the interaction dynamics of the twin-jet plumes and study its associated sound field which exhibits complex radiation characteristics.
