Validation of Noise Reduction Design for Landing Gear in the FQUROH Flight Demonstration Project
Author:
Affiliation:
1. Kawasaki Heavy Industries, Ltd.
2. Japan Aerospace Exploration Agency (JAXA)
Publisher
American Institute of Aeronautics and Astronautics
Reference15 articles.
1. 1Ueno, Y., Nagata, T., Ochi, A., and Hayama, K. "Aeroacoustic Analysis of the Rudimentary Landing Gear Using Octree UnstructuredGrid withBoundary-fittedLayer," AIAAPaper2012-2284,2012.
2. 2Isotani, K., Hayama, K., Yokokawa, Y., Murayama, M., Ura, H., and Yamamoto, K. "An Aerodynamic Noise Reduction StudyforAirframeNoisefromFlapTips,"AIAAPaper2013-2064,2013.
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