Global ETD Search

Search theses and dissertations gathered from participating repositories worldwide. Every result links back to the library that holds it. No account is needed.

Results

Showing 1 to 20 of 62 for “"Aeroacoustic"”.

  1. Physics-based aeroacoustic modelling of bluff-bodies

    … flow solver included a high-order computational aeroacoustics code adopting large-eddy simulation, whilst a Ffowcs Williams and Hawkings solver was used for the acoustic prediction. Circular cylinders in various configurations were selected to represent basic landing gear struts and results were …

    soton Repository record for Physics-based aeroacoustic modelling of bluff-bodies (opens in a new tab)

  2. Aeroacoustic computation of sound radiation from ducts

    … research is being undertaken to understand the aeroacoustic noise source mechanisms and to accurately predict engine noise levels. High-performance computers and advanced numerical techniques are now taking an active role in this research area. In this work, a numerical solver is developed to …

    soton Repository record for Aeroacoustic computation of sound radiation from ducts (opens in a new tab)

  3. Anomaly Detection in Aeroacoustic Wind Tunnel Experiments

    … array, another common system employed in aeroacoustic wind tunnels, will be analyzed similarly through evaluation of the cross-spectral matrix of microphone data, with minimal repeat measurements. A spectral projection method will be proposed that identifies unexpected acoustic source …

    vt Repository record for Anomaly Detection in Aeroacoustic Wind Tunnel Experiments (opens in a new tab)

  4. 2D Aeroacoustic Analysis of Flow in the Flame Trench

    <p>We present here a methodology for using the commercial software ANSYSFLUENT to predict the acoustic field associated with Space-Launch System (SLS). We consider a two-dimensional model of flame deflector, and flame trench. The ANSYS code is then used to simulate the internal flow. Both the …

    embry-riddle Repository record for 2D Aeroacoustic Analysis of Flow in the Flame Trench (opens in a new tab)

  5. Aeroacoustic control of landing gear noise using perforated fairings

    A study was performed to investigate and optimize the application of perforated fairings for landing gear noise control. The sparse knowledge about this new subject has necessitated a more fundamental study involving a basic fairing-strut configuration, followed by wind tunnel tests on a simplified …

    soton Repository record for Aeroacoustic control of landing gear noise using perforated fairings (opens in a new tab)

  6. Accurate aeroacoustic measurements in closed-section hard-walled wind tunnels

    … help in the design of quieter aircraft, however aeroacoustic measurements in wind tunnels are still required. There is a growing interest in simultaneous aerodynamic and aeroacoustic measurements in hard-walled closed-section wind tunnels. The research hypothesis of this work is whether accurate …

    soton Repository record for Accurate aeroacoustic measurements in closed-section hard-walled wind tunnels (opens in a new tab)

  7. Aeroacoustic measurement and analysis of transient supersonic hot nozzle flows

    … were tested at Boeing's steady-state low speed aeroacoustic facility for comparison to the transient shock tube noise data. The assessment establishes the uncertainty bounds on sound pressure level measurements over the range of frequency bands, nozzle pressure ratios (1.5 - 4.0), total …

    mit Repository record for Aeroacoustic measurement and analysis of transient supersonic hot nozzle flows (opens in a new tab)

  8. Computational aeroacoustic modelling using hybrid RANS/LES methods with modified acoustic analogies

    This study considers a numerical approach to identifying noise mechanisms in tandem cylinders to understand aircraft landing gear as a primary contributor to airframe noise during approach and landing. Fluctuations in the flow properties induced by turbulence are computed as well as the …

    cape-town Repository record for Computational aeroacoustic modelling using hybrid RANS/LES methods with modified acoustic analogies (opens in a new tab)

  9. Development of a Plasma Spray Process Monitoring System through Aeroacoustic Signal Analysis

    Plasma spray coatings are vital to the capabilities of jet engines. They allow engines to operate at combustion temperatures that would otherwise melt the superalloy components. Coatings tighten clearance between rotating components, increasing engine compression. They prevent chemical attack and …

    vt Repository record for Development of a Plasma Spray Process Monitoring System through Aeroacoustic Signal Analysis (opens in a new tab)

  10. Aeroacoustic transfer of leading edge serrations from single aerofoils to low-pressure fan applications

    Leading edge serrations are well-known for their aeroacoustic potential in reducing aerofoil-turbulence interaction noise and are also associated with certain aerodynamic advantages. To prepare leading edge serrations for industrial application, two obstacles remain to be addressed. First is a …

    tu-berlin Repository record for Aeroacoustic transfer of leading edge serrations from single aerofoils to low-pressure fan applications (opens in a new tab)

  11. Aerodynamic and aeroacoustic design of small unmanned aircraft system propellers at low Reynolds numbers.

    The Small Unmanned Aircraft System (sUAS) has become an overwhelmingly important asset for military intelligence, surveillance, and reconnaissance in addition to a multitude of needs in the commercial industry. More research should investigate sUAS propulsion systems and specifically the …

    tdl Repository record for Aerodynamic and aeroacoustic design of small unmanned aircraft system propellers at low Reynolds numbers. (opens in a new tab)

  12. Aeroacoustic Study of a Model-Scale Landing Gear in a Semi-Anechoic Wind Tunnel

    An aeroacoustic study was conducted on a 26%-scale Boeing 777 main landing gear in the Virginia Tech (VT) Anechoic Stability Wind Tunnel. The VT Anechoic Stability Wind Tunnel allowed noise measurements to be carried out using both a 63-elements microphone phased array and a linear array of 15 …

    vt Repository record for Aeroacoustic Study of a Model-Scale Landing Gear in a Semi-Anechoic Wind Tunnel (opens in a new tab)

  13. High-Fidelity Modeling of eVTOL Rotor Unsteady Aerodynamic and Aeroacoustic Response to Time-Harmonic Gust

    … This thesis investigates the aerodynamic and aeroacoustic behavior of a representative eVTOL rotor subjected to time-harmonic inflow disturbances, providing a detailed numerical framework to quantify how periodic gusts influence rotor performance, unsteady loading, and sound radiation.</p> …

    embry-riddle Repository record for High-Fidelity Modeling of eVTOL Rotor Unsteady Aerodynamic and Aeroacoustic Response to Time-Harmonic Gust (opens in a new tab)

  14. Aerodynamic and Aeroacoustic Analysis of Low Reynolds Number Propellers Using Higher-Order RANS Transition Turbulence Modeling

    The advent of advanced vehicle concepts involving Urban Air Mobility (UAM) and small Unmanned Aerial Systems (sUAS) has brought about a new class of rotorcraft technology which operate predominantly in low-Reynolds ($Re$) number regimes. In such regimes, the flow experiences complex boundary layer …

    vt Repository record for Aerodynamic and Aeroacoustic Analysis of Low Reynolds Number Propellers Using Higher-Order RANS Transition Turbulence Modeling (opens in a new tab)

  15. Effects of the geometric modifications on the shear layer excitation source in co-axial side branches

    … markedly alter the acoustic field and the aeroacoustic sound source within deep co-axial cavities. Furthermore, it highlights how different upstream distances influence the aeroacoustic resonance of a coaxial side branch and the resultant peak acoustic pressure and the sound source term. …

    uoit Repository record for Effects of the geometric modifications on the shear layer excitation source in co-axial side branches (opens in a new tab)

  16. A measurement based study of the acoustics of pipe systems with flow

    … of this thesis is the measurement of specific aeroacoustic properties in ducts at frequencies below the cut-on frequency of the first higher order mode. A body of measurement results are presented which highlight the effect of flow on some of the aeroacoustic characteristics in ducts as well as …

    soton Repository record for A measurement based study of the acoustics of pipe systems with flow (opens in a new tab)

  17. TIME-CONSERVATIVE FINITE-VOLUME METHOD WITH LARGE-EDDY SIMULATION FOR COMPUTATIONAL AEROACOUSTICS

    … Its applicability to technically relevant aeroacoustic applications is demonstrated. The time-conservative finite-volume method has unique features and advantages in comparison to traditional methods. The main objectives of this study are to develop an advanced, high-resolution, low …

    durham Repository record for TIME-CONSERVATIVE FINITE-VOLUME METHOD WITH LARGE-EDDY SIMULATION FOR COMPUTATIONAL AEROACOUSTICS (opens in a new tab)

  18. Aeroacoustics of perforated drag plates for quiet transport aircraft

    … presented in this thesis focuses primarily on aeroacoustic tests and analysis of perforated drag plates. The idea behind a quiet spoiler or drag rudder is to alter the noise production mechanism by perforating the drag plates. The hypothesis is that the large length scales responsible for the …

    mit Repository record for Aeroacoustics of perforated drag plates for quiet transport aircraft (opens in a new tab)

  19. Fluidic ultrasound generation for nondestructive testing

    … a transient triggered ultrasound pulse based on aeroacoustic sound generation mechanisms in a bistable fluidic amplifier. Little is known about its performance characteristics and suitability for nondestructive testing (NDT). The publications included in this thesis are the first to present a …

    tu-berlin Repository record for Fluidic ultrasound generation for nondestructive testing (opens in a new tab)

Page 1 of 4