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Showing 1 to 14 of 14 for “"Airframe Noise"”.

  1. Clean Wing Airframe Noise Modeling for Multidisciplinary Design and Optimization

    A new noise metric has been developed that may be used for optimization problems involving aerodynamic noise from a clean wing. The modeling approach uses a classical trailing edge noise theory as the starting point. The final form of the noise metric includes characteristic velocity and length …

    vt Repository record for Clean Wing Airframe Noise Modeling for Multidisciplinary Design and Optimization (opens in a new tab)

  2. Multidisciplinary Design Optimization of Low-Noise Transport Aircraft

    … of this research is to examine how to design low-noise transport aircraft using Multidisciplinary Design Optimization (MDO). The subject is approached by designing for low-noise both implicitly and explicitly. The explicit design approach involves optimizing an aircraft while explicitly …

    vt Repository record for Multidisciplinary Design Optimization of Low-Noise Transport Aircraft (opens in a new tab)

  3. Design trade studies and assessment for advanced quiet aircraft concepts

    … for a range of 4,000nm and 250 passengers. A noise assessment was conducted on the engine and airframe noise sources of the resulting design. The noise impacts of five engine (jet, fan forward, fan rearward, core, and turbine) and airframe (airfoil, elevator, slat, drag rudder, and …

    mit Repository record for Design trade studies and assessment for advanced quiet aircraft concepts (opens in a new tab)

  4. Systems analysis of community noise impacts of advanced flight procedures for conventional and hybrid electric aircraft

    … precise navigation technologies have created noise concentration problems for communities beneath flight tracks. There may be opportunities to reduce community noise impacts under these concentrated flight tracks through advanced operational approach and departure procedures and advanced …

    mit Repository record for Systems analysis of community noise impacts of advanced flight procedures for conventional and hybrid electric aircraft (opens in a new tab)

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

    … 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 corresponding …

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

  6. The Computation of Exact Green's Functions in Acoustic Analogy By a Spectral Collocation Boundary Element Method

    <p>Aircraft airframe noise pollution resulting from the take-off and landing of airplanes is a growing concern. Because of advances in numerical analysis and computer technology, most of the current noise prediction methods are computationally efficient. However, the ability to effectively apply an …

    odu Repository record for The Computation of Exact Green's Functions in Acoustic Analogy By a Spectral Collocation Boundary Element Method (opens in a new tab)

  7. Effect of Boundary-Layer Tripping on Turbulence Generation and Trailing-Edge Noise in Transitional Airfoils

    … focus here on attempting to directly predict the noise associated with airframe by considering a single isolated airfoil. Developing an ability to directly predict the radiated noise and how it is generated is a first step for passive or active control of the generated noise. We choose herein a …

    embry-riddle Repository record for Effect of Boundary-Layer Tripping on Turbulence Generation and Trailing-Edge Noise in Transitional Airfoils (opens in a new tab)

  8. Impact of Liquefied Natural Gas usage and payload size on Hybrid Wing Body aircraft fuel efficiency

    … were optimized for reduced fuel burn and airframe noise at approach, based on NASA N+3 goals for the 2030 timeframe. Well-to-wake greenhouse gas emissions for LNG from conventional sources were estimated to be 16% lower than conventional Jet A. Minimally insulated in-wing storage was shown …

    mit Repository record for Impact of Liquefied Natural Gas usage and payload size on Hybrid Wing Body aircraft fuel efficiency (opens in a new tab)

  9. Physics-based aeroacoustic modelling of bluff-bodies

    … this work physics-based modelling of bluff-body noise was performed with application to landing gear noise production. The landing gear is a primary contributor to airframe noise during approach. Noise is primarily generated from the unsteady pressures resulting from the turbulent flow around …

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

  10. Modeling performance and noise of advanced operational procedures for current and future aircraft

    Increasing concerns regarding aircraft noise has encouraged the push to reduce noise via operational adjustments. The objective here is thus to expand analysis capabilities to enable modeling of the impact on aircraft noise due to advanced operational approach procedures, such as delayed …

    mit Repository record for Modeling performance and noise of advanced operational procedures for current and future aircraft (opens in a new tab)

  11. Aerodynamics and aeroacoustics of flap side-edges

    … to the flap side-edge in an attempt to reduce airframe noise. Measurements taken as part of the experimental study were forces, on-surface pressures, particle image velocimetry, hotwire anemometry and on-surface microphones. Oil flow was performed to visualise the on-surface flow. A detached …

    soton Repository record for Aerodynamics and aeroacoustics of flap side-edges (opens in a new tab)

  12. Acoustic Scattering in Sheared Flow

    Airframe noise, the noise of an aircraft in flight not due to the engine or other mechanical devices, is often a major contribution to the sound heard from an aircraft during landing approach. Over the past few decades certification requirements have gradually tightened, reaching the point where …

    cambridge Repository record for Acoustic Scattering in Sheared Flow (opens in a new tab)

  13. Scattering by porous aerofoil adaptations

    … in particular, can generate a large amount of noise that causes disruption and irritation. From the beginning of the jet era, the need to control aeroacoustic noise generation has been important in order to minimise the environmental impact of the aviation industry and its expansion. Sharp …

    cambridge Repository record for Scattering by porous aerofoil adaptations (opens in a new tab)

  14. Numerical investigation of slat noise attenuation using acoustic liners

    Noise generated by high-lift devices such as slats on a wing is a major contributor to the overall airframe noise during the landing approach of a commercial aircraft. In this work the concept of attenuating slat noise using absorptive acoustic liners in the slat/main element gap is explored using …

    soton Repository record for Numerical investigation of slat noise attenuation using acoustic liners (opens in a new tab)