Results 41 to 50 of about 6,709 (233)

Numerical Study on Detonation Initiation Process in Channels Equipped with Typical Ramjet Flameholders

open access: yesAerospace
Differing from traditional isobaric combustion, a pulse detonation-based ramjet (PD-Ramjet) was proposed in this study to enhance the efficiency of traditional ramjets.
Lisi Wei   +3 more
doaj   +1 more source

Ramjet Nozzle Analysis for Transport Aircraft Configuration for Sustained Hypersonic Flight

open access: yesApplied Sciences, 2018
For the past several decades, research dealing with hypersonic flight regimes has been restricted mainly to military applications. Hypersonic transportation could be a possible and affordable solution to travel in the medium term and there is renewed ...
Raman Baidya   +2 more
doaj   +1 more source

Nonlinear analysis of pressure oscillations in ramjet engines [PDF]

open access: yes, 1986
Pressure oscillations in ramjet engines have been studied using an approximate method which treats the flow fields in the inlet and the combustor separately. The acoustic fields in the combustor are expressed as syntheses of coupled nonlinear oscillators
Culick, Fred E. C., Yang, Vigor
core  

A Review of Research on the Thermo‐Force Characteristics of Scramjet Engine Wall Based on Neural Networks

open access: yesInternational Journal of Energy Research, Volume 2025, Issue 1, 2025.
With the development of high‐performance computing and advanced experimental methods, data‐driven machine learning, especially neural network technology, has shown great potential in fluid mechanics research and has become a fourth paradigm research tool.
Chen Qi   +6 more
wiley   +1 more source

Effects of the Air Inlet Angle on the Combustion and Ablation Environment of a Hybrid Powder-Solid Ramjet

open access: yesInternational Journal of Aerospace Engineering, 2022
A hybrid powder-solid ramjet (HPSR) that combined the advantages of a solid rocket ramjet (SRJ) and a powder ramjet engine was investigated in this research.
Jinjin Wang   +4 more
doaj   +1 more source

Tau Zero: In the cockpit of a Bussard ramjet [PDF]

open access: yesAmerican Journal of Physics, 2017
A Bussard ramjet is a relativistic spacecraft, fueled by fusion energy of cosmic matter that is collected during the flight. We derive the equation of motion of such a spaceship for a given mass density in space and the fusion mass defect. Two ramjet engine scenarios, where the thrust for propulsion is generated by emission of photons or acceleration ...
Blatter, Heinz, Greber, Thomas
openaire   +3 more sources

Multiphase Marine Ramjet Using Liquefied Gas as a Source of Bubbles

open access: yesJournal of Marine Science and Engineering, 2020
An innovative variant of a multiphase marine ramjet is investigated analytically and experimentally. Pressure liquefied gas (LG) is injected, boiling under superheat conditions in the water stream within the propulsion unit, and serving as an on-board ...
Herman D. Haustein   +2 more
doaj   +1 more source

The geometric characteristics of the front and the length selection for the combustion chamber of direct flow type

open access: yesАвіаційно-космічна техніка та технологія, 2021
A method has been developed for selecting the geometric characteristics of the front and the length of the direct-flow combustion chamber. Afterburner combustion chambers are of the ramjet type and are used for a short-term increase in the thrust of a ...
Дмитрий Викторович Козел
doaj   +1 more source

A review of the ONR/NAVAIR research option combustion instabilities in compact ramjets, 1983-1988 [PDF]

open access: yes, 1989
This paper consists of two parts summarizing two portions of the ONR/NAVAIR Research Option. The option began in 1983 and continued for five years, involving 11 organizations.
Culick, F. E. C., Schadow, K. C.
core  

A Review on High‐Speed Electromagnetic Flow Control and Applications Considering Numerical Methods, Simulations, and Experimental Research Data

open access: yesInternational Journal of Aerospace Engineering, Volume 2025, Issue 1, 2025.
Background: Electromagnetic flow control is crucial in hypersonic gas dynamics, with key aspects of boundary layer electromagnetic flow control reviewed, focusing on numerical methods, simulations, and experimental research. Numerical Methods: Challenges such as numerical stiffness and instability arise from the coupling of electromagnetic fields with ...
Yang Du, Jun Liu, Hao Chen
wiley   +1 more source

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