Uncertainty analysis and design optimization of solid rocket motors with finocyl grain

Z Hao, L Haowen, W Pengcheng, C Guobiao… - Structural and …, 2020 - Springer
The traditional multidisciplinary design optimization (MDO) method for the conceptual
design of the solid rocket motor (SRM) is usually deterministic and seldom focuses on …

Thermal Requirements for Design and Analysis of Subsonic Single Aft Engine (SUSAN) Research Aircraft

EJ Stalcup, N Heersema - AIAA SCITECH 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-1940. vid The purpose of this
paper is to define a set of thermal requirements which can be used for conceptual design …

[PDF][PDF] Component-led integrative optimisation methodology for avionic thermal management

A Jones - 2017 - core.ac.uk
The modern military aircraft can be defined as a System of Systems (SoS); a number of
distinct systems operating simultaneously across boundary interfaces (Clark 2009). As the …