In-flight thrust determination for high-bypass-ratio turbofan using residual error methodology-Reference-Cited by-同舟云学术

In-flight thrust determination for high-bypass-ratio turbofan using residual error methodology

Published:2018-01-23 Issue:2 Volume:40 Page:
ISSN:1678-5878
Container-title:Journal of the Brazilian Society of Mechanical Sciences and Engineering
language:en
Short-container-title:J Braz. Soc. Mech. Sci. Eng.

Author:

Del Mônaco Monteiro Pedro,Machiaverni Rafael Mattar,Bringhenti Cleverson^ORCID,Tomita Jesuino T.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics

Link

http://link.springer.com/article/10.1007/s40430-018-1012-0/fulltext.html

Reference25 articles.

1. Santos GD (2001) In-flight thrust determination and uncertainty analysis for turbofan engines. MSc Thesis, Instituto Tecnológico de Aeronáutica, São José dos Campos, Brazil

2. Machiaverni RM (2008) Determinação de Tração em Voo através do Método do Erro Eesidual. MSc Thesis in Portuguese, Instituto Tecnológico de Aeronáutica, São José dos Campos, Brazil

3. Mattingly JD (2006) Elements of propulsion: gas turbines and rockets. AIAA Education Series, Published by the American Institute of Aeronautics and Astronautics

4. UNITED STATES (1964) FEDERAL AVIATION ADMINISTRATION. Title 14 code of federal regulations—CFR part 25 airworthiness standards: transport category airplanes. Washington, DC

5. ANAC BRASIL, AGÊNCIA NACIONAL DA AVIAÇÃO CIVÍL (2014) (RBAC) 25:2014: Regulamento Brasileiro da Aviação Civil, Brasilia, DF

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