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Showing 1 to 4 of 4 for “"BEMT"”.

  1. Investigation of the Aerodynamic and Acoustic Performance of a Scaled eVTOL Propeller in Axial and Non-Axial Flight

    … custom-developed Blade Element Momentum Theory (BEMT) utility for low-fidelity predictions. The findings aim to provide baseline data for Computational Fluid Dynamic (CFD) validation, enhancing predictive tools for advancing safe and efficient urban air transportation. Experimental results …

    vt Repository record for Investigation of the Aerodynamic and Acoustic Performance of a Scaled eVTOL Propeller in Axial and Non-Axial Flight (opens in a new tab)

  2. 3D Aerodynamic Optimization of NREL VI Wind Turbine Blade for Increased Power Output and Visualization of Flow Characteristics

    … solver ANSYS 14.5. The power curve obtained from BEMT, Baseline NREL VI CFD Simulations and Optimized Blade Simulations are compared with experimental results. Over prediction is observed in the theoretical result while computational analysis under predicts power produced at post stall region. …

    embry-riddle Repository record for 3D Aerodynamic Optimization of NREL VI Wind Turbine Blade for Increased Power Output and Visualization of Flow Characteristics (opens in a new tab)

  3. Measurement and Prediction of Rotor Noise Sources for sUAS in Outdoor and Laboratory Environments

    … performance and tonal and broadband self-noise. BEMT was used to predict aerodynamic performance. Tonal noise associated with the rotor blade loading and thickness was predicted using F1A and rotor broadband self-noise was predicted using the model of BPM. The measured noise in this facility …

    vt Repository record for Measurement and Prediction of Rotor Noise Sources for sUAS in Outdoor and Laboratory Environments (opens in a new tab)

  4. An investigation of a scalable flight control system for a variable pitch, fuel powered, quad-rotor craft

    Submitted in the fulfillment of requirements of the degree of Master of Mechanical Engineering, Durban University of Technology, Durban, South Africa, 2023.

    dut Repository record for An investigation of a scalable flight control system for a variable pitch, fuel powered, quad-rotor craft (opens in a new tab)