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Showing 1 to 5 of 5 for “"Inlet Flow Distortion"”.

  1. Non-Intrusive Sensing and Feedback Control of Serpentine Inlet Flow Distortion

    … to infer circumferential total pressure distortion intensity found in serpentine inlet airflow was established using wall-pressure fluctuation measurements. This sensing technique was experimentally developed for aircraft with serpentine inlets in a symmetric, level flight condition. The …

    vt Repository record for Non-Intrusive Sensing and Feedback Control of Serpentine Inlet Flow Distortion (opens in a new tab)

  2. Effect of BLI-Type Inlet Distortion on Turbofan Engine Performance

    … ingesting the low velocity boundary layer flow through a serpentine inlet into a turbofan engine adversely affects the performance of the engine. The available literature has only yielded studies of the effects of this specific type of inlet distortion on engine performance in the form of …

    vt Repository record for Effect of BLI-Type Inlet Distortion on Turbofan Engine Performance (opens in a new tab)

  3. An Experimental and Analytical Investigation of Dynamic Flow Response of a Fan Rotor with Distorted Inlet Flow

    … gain insight and ultimately predict the dynamic flow response of a fan rotor with inlet flow distortion. Rotor exit total pressure circumferential profiles were accurately predicted using frequency response functions derived from experimental rotor response data. Using these predicted profiles, …

    vt Repository record for An Experimental and Analytical Investigation of Dynamic Flow Response of a Fan Rotor with Distorted Inlet Flow (opens in a new tab)

  4. An Operational Value Stream Analysis for Developmental Excellence

    … learning models better capture the relevant flow mechanics, improving the circumferential distortion estimations in nacelle aerodynamics by over 10% compared to traditional heuristics. Finally, a CFD-based actuator disk source modeling approach demonstrates a 60% reduction in steady-state …

    mit Repository record for An Operational Value Stream Analysis for Developmental Excellence (opens in a new tab)

  5. Three-dimensional rotating stall inception and effects of rotating tip clearance asymmetry in axial compressors

    The effects of two types of flow nonuniformity on stall inception behavior were assessed with linearized stability analyses of two compressor flow models. Response to rotating tip clearance asymmetries induced by a whirling rotor shaft or rotor height variations were investigated with a …

    mit Repository record for Three-dimensional rotating stall inception and effects of rotating tip clearance asymmetry in axial compressors (opens in a new tab)