A real-time information integration framework for multidisciplinary coupling of complex aircrafts: an application of IIIE

N Li, L Zhao, C Bao, G Gong, X Song, C Tian - Journal of Industrial …, 2021 - Elsevier
Industrial information integration engineering (IIIE) is an interdisciplinary field with the typical
characteristics of enormous and complex systems. As typical enormous and complex …

Three-dimensional adaptive fixed-time cooperative guidance law with impact time and angle constraints

H Yu, K Dai, H Li, Y Zou, X Ma, S Ma… - Aerospace Science and …, 2022 - Elsevier
This paper mainly addresses the simultaneous attack of multiple missiles against a
maneuvering target in three-dimensional (3-D) space. Here, we show that a novel fixed-time …

Preliminary design and test of high altitude two-stage rockets in New Zealand

J Davies, R Grove, T Bell, O Rea, M Furkert… - Aerospace Science and …, 2022 - Elsevier
This article emphasizes the design and development process of a two-stage rocket. The
rocket named Into the Black II (ITBII) is a second-generation rocket at University of …

Aerodynamic Identification and Control Law Design of a Missile Using Machine Learning

L Yan, X Chang, N Wang, L Zhang, W Liu, X Deng - AIAA Journal, 2023 - arc.aiaa.org
The new generation of air vehicle is confronted with a more intricate environment and
challenging missions, which puts forward higher requirements for the flight control system. In …

Numerical investigation of the surface roughness effects on the subsonic flow around a circular cone-cylinder

N Saidi, M Cerdoun, S Khalfallah… - Aerospace Science and …, 2020 - Elsevier
The flow around a circular-cone is 3D, unsteady and turbulent. As reported in many research
works on this type of flow, boundary layer separations, vortex structures and the effect of …

Assessment of Multifidelity Surrogate Approaches for Expedient Loads Prediction in High-Speed Flows

TE Korenyi-Both, JJ McNamara, J Willems Jr… - Journal of Spacecraft …, 2024 - arc.aiaa.org
Fast and accurate predictions about the flowfield surrounding a hypersonic flight vehicle are
necessary for both early design phases and autonomous vehicle control. Data-driven model …

Static aeroelasticity using high fidelity aerodynamics in a staggered coupled and ROM scheme

A Kafkas, G Lampeas - Aerospace, 2020 - mdpi.com
Current technology in evaluating the aeroelastic behavior of aerospace structures is based
on the staggered coupling between structural and low fidelity linearized aerodynamic …

Multi-fidelity multidisciplinary meta-model based optimization of a slender body with fins

S Noureddine, DS Eddine, A Magrini… - Proceedings of the …, 2024 - journals.sagepub.com
Multidisciplinary design optimization (MDO) involving aero-elastic simulations still proves
challenging for computational cost. This paper proposes a competitive cost-effective multi …

Buckling and post-buckling behavior of shell type structures under thermo mechanical loads

ZM Vasić, K Maksimović, MS Maksimović… - Thermal …, 2021 - machinery.mas.bg.ac.rs
The thermo mechanical buckling and post-buckling behavior of layered composite shell type
structure are considered with the finite element method under the combination of …

Aerodynamic‐thermal/structural design optimization of missile fin configuration during supersonic flight condition

B Rašuo, N Vidanović, G Kastratović, N Mirkov - PAMM, 2021 - Wiley Online Library
The main goal of this paper is to expand previously conducted study and consequently to
upgrade the proposed multi‐modular numerical environment developed for fluid‐structure …