Results 71 to 80 of about 845 (188)

Integrating Computer-Aided Design and Model-Based Systems Engineering for Early Zonal Hazard Analysis: Application to a Supersonic Aircraft Fuel System

Aerospace
The development of supersonic aircraft presents significant challenges in ensuring safety during early design stages, particularly for fuel tank systems exposed to extreme thermal and structural loads.
Ayush Kamboj, Yicheng Sun
doaj   +1 more source

Do supersonic aircraft avoid contrails? [PDF]

Atmospheric Chemistry and Physics, 2008
The impact of a potential future fleet of supersonic aircraft on contrail coverage and contrail radiative forcing is investigated by means of simulations with the general circulation model ECHAM4.L39(DLR) including a contrail parameterization.
A. Stenke, V. Grewe, S. Pechtl
doaj  

Installation Effects of Supersonic Inlets on Next-Generation SST Turbofan Engines

Engineering Proceedings
This study explores inlet-related installation effects on next-generation SST aircraft, focusing on supersonic business jets. Using a comprehensive framework with consistent thrust/drag bookkeeping and realistic modeling of inlet losses, including ...
Stylianos Adamidis, Dario Del Gatto, Christos Mourouzidis, Stephen Brown, Vassilios Pachidis   +4 more
doaj   +1 more source

Optimal design for low sonic boom based on CoKriging surrogate model

Hangkong gongcheng jinzhan
Accurately predicting and effectively reducing sonic boom levels is one of the key issues in the development of the new generation of green supersonic civil aircraft.
ZHANG Hanqi, XU Yue, ZHONG Min, LI Yan
doaj   +1 more source

Aerodynamic model identification of supersonic aircraft using Bayesian approach-based Box–Jenkins structure

Alexandria Engineering Journal
Nonlinear aerodynamics complexities of trending supersonic fighter aircraft entail formulation of a robust and reliable System Identification (Sys ID) technique that is capable of giving deep insight into its nonlinear characteristics and being self ...
Muhammad Fawad Mazhar, Muhammad Wasim, Manzar Abbas, Imran Shafi, Jamshed Riaz, Tae-hoon Kim, Imran Ashraf   +6 more
doaj   +1 more source

Cooling Ability/Capacity and Exergy Penalty Analysis of Each Heat Sink of Modern Supersonic Aircraft. [PDF]

Entropy (Basel), 2019
Mao YF, Li YZ, Wang JX, Xiong K, Li JX.
europepmc   +1 more source

Wing structural design of supersonic civil aircraft based on deep neural network

Jixie qiangdu
At present, the research on supersonic civil aircraft wings mainly focuses on the low sonic boom design and supersonic drag reduction technologies. There are relatively few studies on the wing structural design.
NIU Fanggan, MA Wenyuan, YANG Chao, WANG Yu, YIN Hailian   +4 more
doaj  

An MDAO Method for Assessing Benefits of Variable Cycle Engines in the Conceptual Design of Supersonic Civil Aircraft

Aerospace
The Variable Cycle Engine (VCE) is a key enabling technology for addressing the economic and environmental challenges of next-generation supersonic civil aircraft.
Chao Yang, Xiongqing Yu
doaj   +1 more source

Analysis of the Effects of Thermal Environment on Optical Systems for Navigation Guidance and Control in Supersonic Aircraft Based on Empirical Equations. [PDF]

Sensors (Basel), 2016
Cheng X, Yang Y, Hao Q.
europepmc   +1 more source

Airborne Quantum Key Distribution Performance Analysis under Supersonic Boundary Layer. [PDF]

Entropy (Basel), 2023
Yu H, Tang B, Ding H, Xue Y, Tang J, Wang X, Liu B, Shi L.   +7 more
europepmc   +1 more source