Multidisciplinary Design Optimization Framework with Coupled Derivative Computation for Hybrid Aircraft-Reference-Cited by-同舟云学术

Multidisciplinary Design Optimization Framework with Coupled Derivative Computation for Hybrid Aircraft

Published:2020-07 Issue:4 Volume:57 Page:715-729
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Sgueglia Alessandro,Schmollgruber Peter,Bartoli Nathalie,Benard Emmanuel¹,Morlier Joseph²,Jasa John,Martins Joaquim R. R. A.,Hwang John T.³,Gray Justin S.⁴

Affiliation:

1. ISAE-SUPAERO, Université de Toulouse, France

2. University of Toulouse, 31055 Toulouse, France

3. University of California San Diego, La Jolla, California 92093

4. NASA John H. Glenn Research Center, Cleveland, Ohio 44139

Funder

Airbus

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference71 articles.

1. Electric, hybrid, and turboelectric fixed-wing aircraft: A review of concepts, models, and design approaches

2. KirnerR. “An Investigation into the Benefits of Distributed Propulsion on Advanced Aircraft Configurations,” Ph.D. Thesis, Cranfield Univ., Cranfield, England, U.K. 2015.

3. Challenges of future aircraft propulsion: A review of distributed propulsion technology and its potential application for the all electric commercial aircraft

4. Wake ingestion propulsion benefit

5. Performance Analysis of Wake and Boundary-Layer Ingestion for Aircraft Design

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