Large-scale multidisciplinary design optimization of an evtol aircraft using comprehensive analysis

D Saro**i, ML Ruh, AJ Joshy, J Yan, AK Ivanov… - AIAA SciTech 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0146. vid This paper presents a
framework under development for enabling large-scale multi-fidelity modeling and …

Off-nominal performance and reliability of novel aircraft concepts during early design

MV Bendarkar, D Saro**i, DN Mavris - Journal of Aircraft, 2022 - arc.aiaa.org
To achieve improvements in aircraft efficiency and reduced environmental footprint, aircraft
must incorporate novel concepts, architectures, and technologies, such as distributed …

Certification-driven platform for multidisciplinary design space exploration in airframe preliminary design

J **e, D Saro**i, Y Cai, JA Corman, DN Mavris - Journal of Aircraft, 2022 - arc.aiaa.org
Airworthiness certification is a mandatory but expensive process in aircraft development. To
reduce certification cost, it is desired to incorporate certification considerations into aircraft …

Adjoint-based analysis and optimization of beam-like structures subjected to dynamic loads

D Solano, D Saro**i, D Rajaram, DN Mavris - Structural and …, 2022 - Springer
This paper presents the development of a framework to directly size and optimize a structure
under dynamic loads with a special focus on enabling early aircraft design. Low degrees of …

Structural Analysis and Optimization of Wings Subjected to Dynamic Loads

D Saro**i, D Mavris - AIAA Journal, 2022 - arc.aiaa.org
Dynamic loads arising from the Title 14 Code of Federal Regulations (14 CFR;“Aeronautics
and Space,” Federal Aviation Administration, US Dept. of Transportation, Subchapter C …

Evaluation of off-nominal performance and reliability of a distributed electric propulsion aircraft during early design

MV Bendarkar, D Saro**i, E Harrison… - AIAA scitech 2021 …, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-1723. vid General Aviation (GA) is
likely to be at the forefront of a paradigm change in aviation, where the introduction of novel …

Aerostructural predictions combining fenics and a viscous vortex particle method

R Anderson, A Ning, R **ang, SP van Schie… - AIAA SciTech 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-1193. vid Electric Vertical Takeoff
and Landing (eVTOL) aircraft experience complex, unsteady aerodynamic interactions …

Parametric Structural Weight Estimation for the PEGASUS Concept Considering Dynamic Aeroelastic Effects

HD Solano, D Saro**i, JA Corman - AIAA Aviation 2021 Forum, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-3086. vid The Parallel Electric-Gas
Architecture with Synergistic Utilization Scheme (PEGASUS) is currently being investigated …

Structural Layout Design Space Exploration and Structural Sizing of Aircraft Wingbox

D Saro**i, D Solano, DN Mavris - AIAA Scitech 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-1026. vid Structural weight
estimation is an important activity in the aircraft design process. Limited consideration has …

A certification-driven platform for multidisciplinary design space exploration in airframe early preliminary design

D Saro**i, J **e, Y Cai, JA Corman… - AIAA Aviation 2020 …, 2020 - arc.aiaa.org
Following the conceptual phase of aircraft design, sizing and performance estimations shift
from historical-based empirical equations to physics-based simulations. The initial aircraft …