Large-Scale Path-Dependent Optimization of Supersonic Aircraft

Aircraft are multidisciplinary systems that are challenging to design due to interactions between the subsystems. The relevant disciplines, such as aerodynamic, thermal, and propulsion systems, must be considered simultaneously using a path-dependent formulation to assess aircraft performance accura...

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Main Authors: John P. Jasa, Benjamin J. Brelje, Justin S. Gray, Charles A. Mader, Joaquim R. R. A. Martins
Format: Article
Language:English
Published: MDPI AG 2020-10-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/7/10/152
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author John P. Jasa
Benjamin J. Brelje
Justin S. Gray
Charles A. Mader
Joaquim R. R. A. Martins
author_facet John P. Jasa
Benjamin J. Brelje
Justin S. Gray
Charles A. Mader
Joaquim R. R. A. Martins
author_sort John P. Jasa
collection DOAJ
description Aircraft are multidisciplinary systems that are challenging to design due to interactions between the subsystems. The relevant disciplines, such as aerodynamic, thermal, and propulsion systems, must be considered simultaneously using a path-dependent formulation to assess aircraft performance accurately. In this paper, we construct a coupled aero-thermal-propulsive-mission multidisciplinary model to optimize supersonic aircraft considering their path-dependent performance. This large-scale optimization problem captures non-intuitive design trades that single disciplinary models and path-independent methods cannot resolve. We present optimal flight profiles for a supersonic aircraft with and without thermal constraints. We find that the optimal flight trajectory depends on thermal system performance, showing the need to optimize considering the path-dependent multidisciplinary interactions.
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spelling doaj.art-02cd8671d35844369a77de9667d7ff412023-11-20T17:47:58ZengMDPI AGAerospace2226-43102020-10-0171015210.3390/aerospace7100152Large-Scale Path-Dependent Optimization of Supersonic AircraftJohn P. Jasa0Benjamin J. Brelje1Justin S. Gray2Charles A. Mader3Joaquim R. R. A. Martins4Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109, USAAerospace Engineering, University of Michigan, Ann Arbor, MI 48109, USAPSA Branch, NASA John H. Glenn Research Center, Cleveland, OH 44135, USAAerospace Engineering, University of Michigan, Ann Arbor, MI 48109, USAAerospace Engineering, University of Michigan, Ann Arbor, MI 48109, USAAircraft are multidisciplinary systems that are challenging to design due to interactions between the subsystems. The relevant disciplines, such as aerodynamic, thermal, and propulsion systems, must be considered simultaneously using a path-dependent formulation to assess aircraft performance accurately. In this paper, we construct a coupled aero-thermal-propulsive-mission multidisciplinary model to optimize supersonic aircraft considering their path-dependent performance. This large-scale optimization problem captures non-intuitive design trades that single disciplinary models and path-independent methods cannot resolve. We present optimal flight profiles for a supersonic aircraft with and without thermal constraints. We find that the optimal flight trajectory depends on thermal system performance, showing the need to optimize considering the path-dependent multidisciplinary interactions.https://www.mdpi.com/2226-4310/7/10/152multidisciplinary design optimizationtrajectory optimizationaircraft designthermal systems design
spellingShingle John P. Jasa
Benjamin J. Brelje
Justin S. Gray
Charles A. Mader
Joaquim R. R. A. Martins
Large-Scale Path-Dependent Optimization of Supersonic Aircraft
Aerospace
multidisciplinary design optimization
trajectory optimization
aircraft design
thermal systems design
title Large-Scale Path-Dependent Optimization of Supersonic Aircraft
title_full Large-Scale Path-Dependent Optimization of Supersonic Aircraft
title_fullStr Large-Scale Path-Dependent Optimization of Supersonic Aircraft
title_full_unstemmed Large-Scale Path-Dependent Optimization of Supersonic Aircraft
title_short Large-Scale Path-Dependent Optimization of Supersonic Aircraft
title_sort large scale path dependent optimization of supersonic aircraft
topic multidisciplinary design optimization
trajectory optimization
aircraft design
thermal systems design
url https://www.mdpi.com/2226-4310/7/10/152
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