Aeroacoustic Computations of a Transonic Truss-Braced Wing Aircraft: Part 2 – Acoustic Signature and Noise Source Identification-Reference-Cited by-同舟云学术

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Aeroacoustic Computations of a Transonic Truss-Braced Wing Aircraft: Part 2 – Acoustic Signature and Noise Source Identification

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

Ravetta Patricio A.¹,Khorrami Mehdi R.²,Ferris Ryan³

Affiliation:

1. AVEC, Inc.

2. NASA Langley Research Center

3. Dassault Systèmes

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2024-3059

Reference25 articles.

1. [1]Bradley,M.K.,andDroney,C.K."SubsonicUltraGreenAircraftResearch:PhaseIFinalReport,"NASA/CR-2011-216847, April 2011. 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.

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