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Assessment of the Noise Reduction Potential of Advanced Subsonic Transport Concepts for NASA's Environmentally Responsible Aviation Project

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What this work says

Outgoing claims: the papers this work cites, builds on, or argues with.

inferredcites →https://doi.org/10.1115/gt2008-50062openalex-snapshot
An Object-Oriented Computer Code for Aircraft Engine Weight Estimation
inferredcites →https://doi.org/10.1177/1475472x17743659openalex-snapshot
Jet noise shielding provided by a hybrid wing body aircraft
inferredcites →https://doi.org/10.1260/1475-472x.11.3-4.335openalex-snapshot
Propulsion Airframe Aeroacoustic Integration Effects for a Hybrid Wing Body Aircraft Configuration
inferredcites →https://doi.org/10.1260/1475-472x.11.3-4.369openalex-snapshot
Hybrid Wing Body Aircraft System Noise Assessment with Propulsion Airframe Aeroacoustic Experiments
inferredcites →https://doi.org/10.2514/1.9084openalex-snapshot
Design of the Blended Wing Body Subsonic Transport
inferredcites →https://doi.org/10.2514/1.j052540openalex-snapshot
Hybrid Wing–Body Aircraft Slat Noise
inferredcites →https://doi.org/10.2514/3.58586openalex-snapshot
Noise Component Method for Airframe Noise
inferredcites →https://doi.org/10.2514/6.1985-353openalex-snapshot
The influence of camber variation on the aerodynamics of civil transport aircraft
inferredcites →https://doi.org/10.2514/6.1993-2987openalex-snapshot
An overview of recent subsonic laminar flow control flight experiments
inferredcites →https://doi.org/10.2514/6.2002-2openalex-snapshot
Design of the Blended-Wing-Body subsonic transport
inferredcites →https://doi.org/10.2514/6.2003-3213openalex-snapshot
Noise and Flow Studies of Coaxial Jets at Incidence
inferredcites →https://doi.org/10.2514/6.2005-2807openalex-snapshot
Full-Scale Propulsion Airframe Aeroacoustics Investigation
inferredcites →https://doi.org/10.2514/6.2007-4828openalex-snapshot
Subsystem Design and Integration for the More Electric Aircraft
inferredcites →https://doi.org/10.2514/6.2008-5840openalex-snapshot
Advanced PRSEUS Structural Concept Design and Optimization
inferredcites →https://doi.org/10.2514/6.2009-3142openalex-snapshot
Assessment of Soft Vane and Metal Foam Engine Noise Reduction Concepts
inferredcites →https://doi.org/10.2514/6.2009-3144openalex-snapshot
An Analytical Assessment of NASA's N+1 Subsonic Fixed Wing Project Noise Goal
inferredcites →https://doi.org/10.2514/6.2009-931openalex-snapshot
Hybrid Wing Body Configuration System Studies
inferredcites →https://doi.org/10.2514/6.2009-933openalex-snapshot
Blended-Wing-Body Low-Speed Flight Dynamics: Summary of Ground Tests and Sample Results (Invited)
inferredcites →https://doi.org/10.2514/6.2009-935openalex-snapshot
Blended-Wing-Body Transonic Aerodynamics: Summary of Ground Tests and Sample Results (Invited)
inferredcites →https://doi.org/10.2514/6.2011-2854openalex-snapshot
Design of the Next Generation Aircraft Noise Prediction Program: ANOPP2
inferredcites →https://doi.org/10.2514/6.2012-2194openalex-snapshot
Evaluation of Parallel-Element, Variable-Impedance, Broadband Acoustic Liner Concepts
inferredcites →https://doi.org/10.2514/6.2012-2669openalex-snapshot
Experimental Investigation of the Low-Speed Aerodynamic Characteristics of a 5.8-Percent Scale Hybrid Wing Body Configuration
inferredcites →https://doi.org/10.2514/6.2012-547openalex-snapshot
Application of Cart3D to Complex Propulsion-Airframe Integration with Vehicle Sketch Pad
inferredcites →https://doi.org/10.2514/6.2013-2185openalex-snapshot
Open Rotor Installed Aeroacoustic Testing with Conventional and Unconventional Airframes
inferredcites →https://doi.org/10.2514/6.2013-541openalex-snapshot
High Bypass Ratio Jet Noise Reduction and Installation Effects Including Shielding Effectiveness
inferredcites →https://doi.org/10.2514/6.2014-0257openalex-snapshot
Noise and Fuel Burn Reduction Potential of an Innovative Subsonic Transport Configuration
inferredcites →https://doi.org/10.2514/6.2014-0365openalex-snapshot
On Noise Assessment for Blended Wing Body Aircraft
inferredcites →https://doi.org/10.2514/6.2014-2478openalex-snapshot
Aeroacoustic Evaluation of Flap and Landing Gear Noise Reduction Concepts
inferredcites →https://doi.org/10.2514/6.2014-2480openalex-snapshot
Towards Full Aircraft Airframe Noise Prediction: Detached Eddy Simulations
inferredcites →https://doi.org/10.2514/6.2014-2624openalex-snapshot
Shielding of Turbomachinery Broadband Noise from a Hybrid wing Body Aircraft Configuration
inferredcites →https://doi.org/10.2514/6.2014-2625openalex-snapshot
Jet Noise Shielding Provided by a Hybrid Wing Body Aircraft
inferredcites →https://doi.org/10.2514/6.2014-2626openalex-snapshot
Noise Scaling and Community Noise Metrics for the Hybrid Wing Body Aircraft
inferredcites →https://doi.org/10.2514/6.2014-3275openalex-snapshot
Aerodynamic Shape Optimization of an Adaptive Morphing Trailing Edge Wing
inferredcites →https://doi.org/10.2514/6.2015-2325openalex-snapshot
Hybrid Wing Body (HWB) Aircraft Design and Optimization using Stitched Composites
inferredcites →https://doi.org/10.2514/6.2015-2987openalex-snapshot
An Assessment of Flap and Main Landing Gear Noise Abatement Concepts
inferredcites →https://doi.org/10.2514/6.2015-2988openalex-snapshot
Evaluation of Airframe Noise Reduction Concepts via Simulations Using a Lattice Boltzmann Approach
inferredcites →https://doi.org/10.2514/6.2015-3289openalex-snapshot
Evaluation of Adaptive Compliant Trailing Edge Technology
inferredcites →https://doi.org/10.2514/6.2016-0007openalex-snapshot
Overview Of ERA Integrated Technology Demonstration (ITD) 51A Ultra-High Bypass (UHB) Integration for Hybrid Wing Body (HWB) (Invited)
inferredcites →https://doi.org/10.2514/6.2016-0056openalex-snapshot
An Overview of Active Flow Control Enhanced Vertical Tail Technology Development
inferredcites →https://doi.org/10.2514/6.2016-0804openalex-snapshot
Evaluation of Load Analysis Methods for NASA’s GIII Adaptive Compliant Trailing Edge Project
inferredcites →https://doi.org/10.2514/6.2016-0864openalex-snapshot
Innovative Flow Control Concepts for Drag Reduction
inferredcites →https://doi.org/10.2514/6.2016-1030openalex-snapshot
Assessment of the Performance Potential of Advanced Subsonic Transport Concepts for NASA’s Environmentally Responsible Aviation Project
inferredcites →https://doi.org/10.2514/6.2016-1273openalex-snapshot
Landing Gear Noise Prediction and Analysis for Tube-And-Wing and Hybrid-Wing-Body Aircraft
inferredcites →https://doi.org/10.2514/6.2016-2957openalex-snapshot
Modeling and Prediction of Krueger Device Noise

What points at this work

Incoming claims: where this work appears in other papers’ reference lists and arguments.

inferred← citeshttps://doi.org/10.2139/ssrn.5087765openalex-extracted
Data in Brief : Conceptual Design-Optimisation of a Subsonic Hydrogen-Powered Longrange Blended-Wing-Body Aircraft
inferred← citeshttps://doi.org/10.1007/s13272-019-00371-8openalex-snapshot
Advanced low-noise aircraft configurations and their assessment: past, present, and future
inferred← citeshttps://doi.org/10.1007/s13272-019-00373-6openalex-snapshot
Auralization of air vehicle noise for community noise assessment
inferred← citeshttps://doi.org/10.1007/s42405-023-00674-5openalex-snapshot
Optimization Design and Analysis of Power Management for Serial Hybrid-Electric Propulsion System Under Aircraft/Engine Integrated Framework
inferred← citeshttps://doi.org/10.1016/j.ast.2021.107101openalex-snapshot
Deep learning based multistage method for inverse design of supercritical airfoil
inferred← citeshttps://doi.org/10.1016/j.ast.2021.107227openalex-snapshot
Series-hybridisation, distributed electric propulsion and boundary layer ingestion in long-endurance, small remotely piloted aircraft: Fuel consumption improvements
inferred← citeshttps://doi.org/10.1016/j.ijhydene.2024.10.329openalex-snapshot
Conceptual design-optimisation of a future hydrogen-powered ultrahigh bypass ratio geared turbofan engine
inferred← citeshttps://doi.org/10.1016/j.paerosci.2024.100996openalex-snapshot
Slat noise in high-lift systems
inferred← citeshttps://doi.org/10.1051/aacus/2023009openalex-snapshot
Conceptual estimation of the noise reduction potential of electrified aircraft engines
inferred← citeshttps://doi.org/10.1051/jnwpu/20224020352openalex-snapshot
Investigation on the flow mechanism of nacelle airframe interaction for podded blended wing body transport
inferred← citeshttps://doi.org/10.1115/gt2019-91432openalex-snapshot
Using Machine Learning to Predict Core Sizes of High-Efficiency Turbofan Engines
inferred← citeshttps://doi.org/10.1177/1475472x221107369openalex-snapshot
Systematic validation of the PAAShA shielding prediction method
inferred← citeshttps://doi.org/10.1177/1475472x261419084openalex-snapshot
Airframe scattering of engine fan noise
inferred← citeshttps://doi.org/10.2514/1.c035307openalex-snapshot
Far Term Noise Reduction Roadmap for the Mid-Fuselage Nacelle Subsonic Transport
inferred← citeshttps://doi.org/10.2514/1.c036124openalex-snapshot
Comparative Assessment of Aircraft System Noise Simulation Tools
inferred← citeshttps://doi.org/10.2514/1.c036259openalex-snapshot
Aircraft System Noise of the NASA D8 Subsonic Transport Concept
inferred← citeshttps://doi.org/10.2514/1.c037332openalex-snapshot
Assessment of an Open-Source Aircraft Noise Prediction Model Using Approach Phase Measurements
inferred← citeshttps://doi.org/10.2514/1.j066372openalex-snapshot
Landing Gear Wheel Hub-Cavity Noise Passive Control Using Novel Sonic Black Hole
inferred← citeshttps://doi.org/10.2514/6.2014-2478openalex-snapshot
Aeroacoustic Evaluation of Flap and Landing Gear Noise Reduction Concepts
inferred← citeshttps://doi.org/10.2514/6.2016-0007openalex-snapshot
Overview Of ERA Integrated Technology Demonstration (ITD) 51A Ultra-High Bypass (UHB) Integration for Hybrid Wing Body (HWB) (Invited)
inferred← citeshttps://doi.org/10.2514/6.2016-0056openalex-snapshot
An Overview of Active Flow Control Enhanced Vertical Tail Technology Development
inferred← citeshttps://doi.org/10.2514/6.2016-1030openalex-snapshot
Assessment of the Performance Potential of Advanced Subsonic Transport Concepts for NASA’s Environmentally Responsible Aviation Project
inferred← citeshttps://doi.org/10.2514/6.2016-1273openalex-snapshot
Landing Gear Noise Prediction and Analysis for Tube-And-Wing and Hybrid-Wing-Body Aircraft
inferred← citeshttps://doi.org/10.2514/6.2016-2906openalex-snapshot
Auralization of NASA N+2 Aircraft Concepts from System Noise Predictions
inferred← citeshttps://doi.org/10.2514/6.2016-2907openalex-snapshot
A Psychoacoustic Evaluation of Noise Signatures from Advanced Civil Transport Aircraft
inferred← citeshttps://doi.org/10.2514/6.2016-3039openalex-snapshot
Potential for Landing Gear Noise Reduction on Advanced Aircraft Configurations
inferred← citeshttps://doi.org/10.2514/6.2016-3040openalex-snapshot
Progress of Aircraft System Noise Assessment with Uncertainty Quantification for the Environmentally Responsible Aviation Project
inferred← citeshttps://doi.org/10.2514/6.2016-3041openalex-snapshot
Quantification of Acoustic Scattering Prediction Uncertainty for Aircraft System Noise Assessment
inferred← citeshttps://doi.org/10.2514/6.2017-3193openalex-snapshot
Aircraft Noise Reduction Technology Roadmap Toward Achieving The NASA 2035 Goal
inferred← citeshttps://doi.org/10.2514/6.2017-3194openalex-snapshot
Ground Noise Contour Prediction for A NASA Hybrid Wing Body Subsonic Transport Aircraft
inferred← citeshttps://doi.org/10.2514/6.2018-0521openalex-snapshot
Achievement of NASA New Aviation Horizons N+2 Goals with a Blended-Wing-Body X-Plane Designed for the Regional Jet and Single-Aisle Jet Markets
inferred← citeshttps://doi.org/10.2514/6.2018-3124openalex-snapshot
Aircraft System Noise Assessment of the NASA D8 Subsonic Transport Concept
inferred← citeshttps://doi.org/10.2514/6.2018-3127openalex-snapshot
Opportunities and Challenges for X-plane Acoustic Flight Research
inferred← citeshttps://doi.org/10.2514/6.2019-2428openalex-snapshot
Far Term Noise Reduction Technology Roadmap for a Large Twin-Aisle Tube-and-Wing Subsonic Transport
inferred← citeshttps://doi.org/10.2514/6.2019-2539openalex-snapshot
The Aircraft Noise Simulation Working Group (ANSWr) - Tool Benchmark and Reference Aircraft Results
inferred← citeshttps://doi.org/10.2514/6.2019-2564openalex-snapshot
Effect of Grazing Flow on Grooved Over-the-Rotor Acoustic Casing Treatments
inferred← citeshttps://doi.org/10.2514/6.2019-2610openalex-snapshot
On Aircraft Trailing Edge Noise
inferred← citeshttps://doi.org/10.2514/6.2020-2582openalex-snapshot
A Comparison of Aircraft Flyover Auralizations by the Aircraft Noise Simulation Working Group
inferred← citeshttps://doi.org/10.2514/6.2022-2993openalex-snapshot
Propulsion Airframe Aeroacoustics and Aircraft System Noise Flight Research Test: NASA Overview
inferred← citeshttps://doi.org/10.2514/6.2022-2996openalex-snapshot
Fan Acoustic Flight Effects on the PAA & ASN Flight Test
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