Aeroacoustic Computations of a Transonic Truss-Braced Wing Aircraft: Part 1 – Aerodynamic and Airframe Noise Simulations-Reference-Cited by-同舟云学术

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Aeroacoustic Computations of a Transonic Truss-Braced Wing Aircraft: Part 1 – Aerodynamic and Airframe Noise Simulations

Published:2024-05-30 Issue: Volume: Page:
ISSN:
Container-title:30th AIAA/CEAS Aeroacoustics Conference (2024)
language:
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Author:

Ferris Ryan¹,Khorrami Mehdi R.²

Affiliation:

1. Dassault Systemes Americas Corp

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2024-3058

Reference38 articles.

1. [1]Bradley, M.K.,andDroney, C. K."SubsonicUltraGreenAircraft Research:Phase IFinalReport," NASA/CR 2011-216847, April2011.URLhttps://ntrs.nasa.gov/citations/20110011321.

2. [2]Bradley,M.K.,Droney,C.K.,andAllen,T.,T."SubsonicUltraGreenAircraftResearch:PhaseII-VolumeI-TrussBraced WingDesignExploration,"NASA/CR-2015-218704/VolumeI,April2015.URLhttps://ntrs.nasa.gov/citations/20150017036.

3. Harrison, N. A., Beyar, M., Dickey, E. D., Hoffman, K., E. Y.Gatlin, G. M., and Viken, S. A. "Development of an Efficient M=0.80TransonicTruss-BracedWingAircraft," AIAAPaper2020-0011,January2020.doi:10.2514/6.2020-0011.

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1. Aeroacoustic Computations of a Transonic Truss-Braced Wing Aircraft: Part 2 – Acoustic Signature and Noise Source Identification;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

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