Effect of nacelle orientation on the aerodynamic characteristics of an arrow wing-body configuration at Mach number 2.03
Engine nacelle orientation effect on aerodynamic characteristics of arrow wing body configuration
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Engine nacelle orientation effect on aerodynamic characteristics of arrow wing body configuration
Pressure distribution at supersonic speeds on conically cambered wing with and without pylon mounted engine nacelles
Transonic wind tunnel study of control span and large wing-tip nacelles results on effectiveness of spoiler-slot-deflector controls on fighter aircraft
Aft-fuselage-mounted nacelles effect on subsonic longitudnal aerodynamic characteristics of twin turbojet aircraft
The spatial structure of turbulence in atmospheric boundary layer flows is highly relevant to wind energy. In particular, wind turbine control strategies based on inflow preview measurements require knowledge of the longitudinal evolution of turbulent flow as it approaches the rotor. These upstream measurements are usually obtained with nacelle-mounted wind lidars. In contrast to traditional in situ anemometry, lidars collect measurements within a probe volume which varies in size depending on the technology of the commercial system being used. Here, we address two issues related to the use of wind lidar to measure the incoming flow to a wind turbine: (i) whether existing longitudinal coherence models can be used to predict flow at the rotor, based on measurements performed at a distance away from the rotor; and (ii) what effect probe-volume averaging has on the inflow predictions. These two questions are critical to the design and implementation of robust wind turbine control strategies. To address these questions, we perform field measurements and large-eddy simulations to determine which incoming flow structures can be readily predicted with existing coherence models, and which require additional corrections to account for lidar volumetric averaging effects. Results reveal that the wind turbine induction zone has a negligible impact on the longitudinal coherence and first-order turbulence quantities, such as the standard deviation of velocity fluctuations. However, the phase of the signal, from which advection time periods of the turbulent structures are derived, is affected by the rotor blockage effect.
In large wind plants, wakes from upwind turbines affect downwind turbines by reducing wind speeds and increasing turbulence. Wake steering may mitigate this effect by deflecting the wakes of upwind turbines away from downwind units. Here, we characterize the impact of wakes from yawed turbines at a commercial-scale wind plant under varying atmospheric and turbine operating conditions. Six months of nacelle-based lidar measurements were collected as part of a field campaign in 2019-2020 in the northern US Great Plains to test the effectiveness of wake steering. We separate these lidar scans by atmospheric stability and turbine operating condition to summarize how yawed wind turbine wakes vary with these input parameters in the atmospheric boundary layer. We summarize the impact of wake steering on various wake characteristics including velocity deficit, wake width, and wake center as retrieved from these lidar data. Yawed wakes have significantly different centerline characteristics compared to unyawed wakes, with large regions of meander in the mid wake region. Yawed wakes are also deflected farther than unyawed wakes in less turbulent conditions with velocity deficits persisting further downstream in stable atmospheric conditions. Overall, yawed wind turbine wakes are larger and wider in lower wind speed environments, and yawed wakes are deflected farther in less turbulent conditions, suggesting that wake steering is most effective in stable atmospheric stratification.
Test data from the National Wind Technology Center (NWTC) for the WindCube Nacelle Lidar. Includes both real-time and 10-minute average data.
Jet wake effect of high bypass jet engine on wing-nacelle interference drag of subsonic transport model
Wind tunnel tests of airframe installation effects on F-106B scale model with simulated underwing engine nacelles at Mach 0.56 to 1.46
Nacelle treatment using broad band resonator for turbofan engine from aerodynamic and acoustical criteria
NASA nacelle acoustic treatment program and flyover noise prediction method
Design modifications for acoustically absorbing flight test nacelles of DC-8 turbofan engine
Noise predictions and economics of nacelle modifications to DC-8 aircraft
Noise level predictions and economics of Boeing nacelle modifications
Numerical method for evaluation and utilization of supersonic nacelle-wing interference
NASA acoustically treated nacelle program to reduce jet aircraft noise
Airframe installation effects on variable flap ejector nozzle of underwing engine nacelle
Nacelle induced flutter effects in elastodynamic scaled model of fan jet transport aircraft mounted in wind tunnel