[HTML][HTML] Multidisciplinary optimization of aircraft aerodynamics for distributed propulsion configurations

S Luo, TZ Eng, Z Tang, Q Ma, J Su, G Bugeda - Applied Sciences, 2024 - mdpi.com
The combination of different aerodynamic configurations and propulsion systems, namely,
aero-propulsion, affects flight performance differently. These effects are closely related to …

Aerodynamic/stealth design of S-duct inlet based on discrete adjoint method

J Deng, K Zhao, L Zhou, W Zhang, B Shu… - Applied Mathematics …, 2024 - Springer
It is a major challenge for the airframe-inlet design of modern combat aircrafts, as the flow
and electromagnetic wave propagation in the inlet of stealth aircraft are very complex. In this …

Adaptive Design Method for a Tilt-Rotor Engine Inlet Duct Optimization

B Soemarwoto, R Habing, M Pecoraro - AIAA AVIATION 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-4019. vid An adaptive design
methodology is presented involving an inverse design to obtain the most possible favorable …

Aerodynamic Characteristics of a Blended-Wing-Body Aircraft With A Serpentine Inlet Using Flow Control Techniques

MS Youn, YJ Kim - Turbo Expo: Power for Land, Sea …, 2021 - asmedigitalcollection.asme.org
Demands of a modern aircraft regarding its aerodynamic performance and high efficiency
are ever-growing. An S-shaped inlet, as known as a serpentine duct, plays a significant role …

Structural design of a morphing serpentine inlet using a multi-material topology optimization methodology

E Munroe, R Bohrer, WA Chishty, IY Kim - Structural and Multidisciplinary …, 2021 - Springer
A promising avenue for development in the aerospace industry involves relocation of
engines from conventional locations beneath the wings, to within the aircraft fuselage …

Response surface optimization of serpentine air inlet ducts in modern fighters

ÖF Yahşi - 2023 - open.metu.edu.tr
Modern fighter aircraft design necessitates improved stealth characteristics in terms of radar
observability. Integration of a lengthy, convoluted air intake duct to aircraft, which plays a …

Aerodynamic Optimisations of Vortex Generators on a Wind Turbine Aerofoil using an Adjoint Solver

A Conchello, X Shen, C Zhu, L Yang… - 2022 7th International …, 2022 - ieeexplore.ieee.org
The adjoint solver (AS) is a relatively new tool with a lot of potential which can optimise a
plethora of flow observables in a faster and more automatic manner than other methods …