Results 41 to 50 of about 16,840 (258)
Aerospace, 2023 Supersonic combustion instability studies are crucial for the future maturation of scramjet engines. In the present paper, the supersonic combustion instability in a strut-based scramjet combustor is investigated through large eddy simulation and dynamic
Yuwei Cheng +3 more
doaj +1 more source
A Mixing Process Influenced by Wall Jet-Induced Shock Waves in Supersonic Flow
Applied Sciences, 2022 With the development of hypersonic air-breathing propulsion systems, such as the supersonic combustion ramjet (Scramjet) and rocket-based combined cycle (RBCC) engines, the mixing process of supersonic airstream with fuel in the engine combustor has been
Ji Zhang +3 more
doaj +1 more source
Leading-to-trailing edge theoretical design of a generic scramjet
AIP Advances, 2022 The aerospace vehicle flying at hypersonic speed, using an airbreathing propulsion system based on supersonic combustion (scramjet) technology, requires a highly integrated system without moving parts, making the propulsion system and vehicle shape ...
R. Carneiro +5 more
semanticscholar +1 more source
Wavelet-based Adaptive Techniques Applied to Turbulent Hypersonic Scramjet Intake Flows
, 2013 The simulation of hypersonic flows is computationally demanding due to large gradients of the flow variables caused by strong shock waves and thick boundary or shear layers.
Behr, Marek +4 more
core +1 more source
Medium independent jet (MI-Jet) engine
Propulsion and Power Research, 2020 MI-Jet or medium independent jet engine is a new conceptual design which can be used in any gaseous atmosphere or in any planets with an ISP greater than that of the existing rocket engines.
Prajith Kumar K P, Aravind Vaidyanathan
doaj +1 more source
Numerical study of detonation wave propagation modes in annular channels
AIP Advances, 2021 Modes of detonation wave propagation in annular channels were investigated numerically by using the adaptive mesh refinement technique. Two-dimensional, reactive Euler equations with a detailed hydrogen/oxygen reaction model were adopted in the ...
Duo Zhang +6 more
doaj +1 more source
Investigation of the Flow In Cold Condition at the Exit of a Supersonic Combustor Test Bench [PDF]
Journal of Aerospace Technology and Management, 2020 For studies of hypersonic flows and supersonic combustion in ground test facilities, three devices can be used as ram accelerators, shock tunnels and supersonic combustor test benches.
Jefte da Silva Guimarães +3 more
doaj +1 more source
International Journal of Applied Ceramic Technology, Volume 23, Issue 1, February 2026.Abstract Novel compositionally complex borides, (Hf,Zr,Nb,Ti)B2 and (Hf,Zr,Nb,Ti)B2‒LaB6, were fabricated using spark plasma sintering process. (Hf,Zr,Nb,Ti)B2‒LaB6 exhibits a dual‐phase microstructure, in which (Hf,Zr,Nb,Ti)B2 is a primary phase with the hexagonal structure and LaB6 is a secondary phase with a cubic structure.
Xin Chen +8 more
wiley +1 more source
Chemistry–Methods, Volume 6, Issue 1, January 2026.A high‐pressure shock‐tube facility is developed to investigate high‐temperature chemical‐kinetics for next‐generation combustion systems. The design enables extended test times and integrates multiple optical diagnostics for time‐resolved species detection.
Sulaiman A. Alturaifi +8 more
wiley +1 more source
Continuous and Discrete Adjoints to the Euler Equations for Fluids
, 2011 Adjoints are used in optimization to speed-up computations, simplify optimality conditions or compute sensitivities. Because time is reversed in adjoint equations with first order time derivatives, boundary conditions and transmission conditions through ...
Alauzet, Frederic, Pironneau, Olivier
core +1 more source