Probabilistic margin assessment of aircraft conceptual design using a modified reliability based design optimization methodology
Probabilistic margin assessment of aircraft conceptual design using a modified reliability based design optimization methodology
The work proposes a Modified Reliability Based Design Optimization (MRBDO) methodology for assessing margins assigned to uncertain parameters during the aircraft conceptual design. The MRBDO approach consists in integrating the concept of margins into the traditional RBDO approach to identify optimized aircraft design while considering the constraint of a required confidence level of achieving performance targets. For the overall aircraft design, we consider stretching a civil medium-range aircraft with the uncertainties in structural weight, aerodynamic performance and propulsion system as a case study. The reliability index associated to the range of the aircraft is evaluated from the uncertainties of OWE, L/D and SFC perturbations. The case study shows that this MRBDO method can effectively determine the optimal safety factors of the aircraft design range for a pre-set confidence level. Compared to that using the classical approach, the maximum take-off weight of the aircraft is reduced by 3.3%.
4463-4477
Yuan, Jie
4bcf9ce8-3af4-4009-9cd0-067521894797
Savill, M.
4c68e863-c14a-41dc-85dd-1ee8220fa09d
Kipouros, T.
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Coggon, S.
efa380bc-99e3-4c60-8750-1beb963db423
Scarpa, F.
684472c3-1a28-478a-a388-5fd896986c1d
21 September 2016
Yuan, Jie
4bcf9ce8-3af4-4009-9cd0-067521894797
Savill, M.
4c68e863-c14a-41dc-85dd-1ee8220fa09d
Kipouros, T.
2b21bdc0-eba1-44b7-98cb-4d69a9d14f87
Coggon, S.
efa380bc-99e3-4c60-8750-1beb963db423
Scarpa, F.
684472c3-1a28-478a-a388-5fd896986c1d
Yuan, Jie, Savill, M., Kipouros, T., Coggon, S. and Scarpa, F.
(2016)
Probabilistic margin assessment of aircraft conceptual design using a modified reliability based design optimization methodology.
Sas, Paul, Moens, David and van de Walle, Axel
(eds.)
In Proceedings of ISMA 2016 - International Conference on Noise and Vibration Engineering and USD2016 - International Conference on Uncertainty in Structural Dynamics.
.
Record type:
Conference or Workshop Item
(Paper)
Abstract
The work proposes a Modified Reliability Based Design Optimization (MRBDO) methodology for assessing margins assigned to uncertain parameters during the aircraft conceptual design. The MRBDO approach consists in integrating the concept of margins into the traditional RBDO approach to identify optimized aircraft design while considering the constraint of a required confidence level of achieving performance targets. For the overall aircraft design, we consider stretching a civil medium-range aircraft with the uncertainties in structural weight, aerodynamic performance and propulsion system as a case study. The reliability index associated to the range of the aircraft is evaluated from the uncertainties of OWE, L/D and SFC perturbations. The case study shows that this MRBDO method can effectively determine the optimal safety factors of the aircraft design range for a pre-set confidence level. Compared to that using the classical approach, the maximum take-off weight of the aircraft is reduced by 3.3%.
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Published date: 21 September 2016
Venue - Dates:
27th International Conference on Noise and Vibration Engineering, Katholieke Universiteit Leuven, Leuven, Belgium, 2016-09-19 - 2016-09-21
Identifiers
Local EPrints ID: 479213
URI: http://eprints.soton.ac.uk/id/eprint/479213
PURE UUID: 77bc91f6-a719-49b3-a2c8-d40cb2337b33
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Date deposited: 20 Jul 2023 16:45
Last modified: 21 Jul 2023 02:02
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Contributors
Author:
Jie Yuan
Author:
M. Savill
Author:
T. Kipouros
Author:
S. Coggon
Author:
F. Scarpa
Editor:
Paul Sas
Editor:
David Moens
Editor:
Axel van de Walle
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