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System Noise Assessment and Uncertainty Analysis of a Conceptual Supersonic Aircraft

This paper describes a system noise assessment of a conceptual supersonic aircraft called the NASA 55t Supersonic Technology Concept Aeroplane (STCA), its prediction uncertainty, and related validation tests. A landing and takeoff noise (LTO) standard for supersonic aircraft is needed to realize fut...

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Autori principali: Junichi Akatsuka, Tatsuya Ishii
Natura: Artigo
Lingua:Inglês
Pubblicazione: MDPI AG 2022-04-01
Serie:Aerospace
Soggetti:
aircraft noise prediction
noise certification
supersonic aircraft
NASA STCA
ICAO Annex 16 Vol.1
Accesso online:https://www.mdpi.com/2226-4310/9/4/212
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