PhD, University of Cincinnati, 2021, Engineering and Applied Science: Aerospace Engineering
In streamlined airplane configurations, additional noise sources can be created from interactions between the jet flow and surfaces on an aircraft's body. During takeoff and landing procedures the ground itself is close enough to already cause jet-surface interference. During these procedures, workers on an aircraft carrier are exposed to such noise radiation and can suffer from varying degrees of hearing loss, providing an impetus from the Navy to study these conditions. To assess this interaction, the presence of a flat plate impinging on a supersonic jet of a low aspect ratio (2:1) rectangular nozzle of equivalent exit diameter of De=20.65mm, is studied from the minor and major axis orientation. The impact of the plate, large enough in length to resemble an aircraft carrier deck relative to the nozzle in scale, is studied at supersonic nozzle pressure ratios (NPRs) of 2.5–4.5. These surface interactions have been studied in large part on cold jets to a certain extent, as these are more easily replicated in a laboratory setting. However more realistic applications involve a heated jet flow, particularly in Navy jet applications. This leads to tested operating conditions produced here of the cold flow temperature ratio (TR=1.0) to a heated jet up to TR=3.0.
To investigate this application, acoustic data from near-field and far-field arrays is captured, and combined with visual flow measurements from streamwise particle image velocimetry (PIV) and shadowgraph/Schlieren photography. From PIV data, average velocity and turbulence kinetic energy (TKE) of the flow can be extracted, while shadowgraph provides various density gradients across the flow field. Further processing in the form of proper orthogonal decomposition (POD) can be applied here to extract dominant modes of the jet's movement. Plate offset (h) distances of h/De=?0, 1, 2, and 3 from the nozzle lip are studied to assess trends related to shock cell spacing, potential core length, and shear layer devel (open full item for complete abstract)
Committee: Ephraim Gutmark Ph.D. (Committee Chair); Shaaban Abdallah Ph.D. (Committee Member); Jeffrey Kastner Ph.D. (Committee Member); Mark Turner Sc.D. (Committee Member)
Subjects: Aerospace Materials