Ground Noise Contour Prediction for A NASA Hybrid Wing Body Subsonic Transport Aircraft
Author:
Affiliation:
1. NASA Langley Research Center
2. NEAT Consulting
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3194
Reference11 articles.
1. Nickol, C.L., and Haller, W.J. "Assessment of the Fuel Burn Reduction Potential of Advanced Subsonic Transport Concepts for NASA's Environmentally Responsible Aviation Project," AIAA Paper 2016-1030.
2. Thomas, R.H., Burley, C.L., and Nickol, C.L. "Assessment of the Noise Reduction Potential of Advanced Subsonic Transport Concepts for NASA's Environmentally Responsible Aviation Project," AIAA Paper 2016-0863.
3. Thomas, R.H., Burley, C.L., and Guo, Y. "Progress of Aircraft System Noise Assessment with Uncertainty Quantification for the Environmentally Responsible Aviation Project," AIAA 2016-3040.
4. Hybrid Wing Body Aircraft System Noise Assessment with Propulsion Airframe Aeroacoustic Experiments
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