Review of combustion stabilization for hypersonic airbreathing propulsion

Q Liu, D Baccarella, T Lee - Progress in Aerospace Sciences, 2020 - Elsevier
A review of fundamental research in combustion stabilization for hypersonic airbreathing
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …

Effect of Plasma Sheaths on Earth-Entry Magnetohydrodynamics

B Parent, PT Rajendran, SO Macheret, J Little… - … of thermophysics and …, 2023 - arc.aiaa.org
The first study of the full coupling between the aerothermodynamics, the
magnetohydrodynamics (MHD), and the plasma sheaths within Earth-entry flows is here …

Expansion tube magnetohydrodynamic experiments with argon test gas

DE Gildfind, D Smith, SW Lewis, R Kelly… - 2018 Flow Control …, 2018 - arc.aiaa.org
In this study an expansion tube is used to generate an experiment to study and evaluate the
concept of magnetohydrodynamic aerobraking for planetary entry spacecraft. An expansion …

Expansion tube test flow design for magnetohydrodynamic aerobraking

DE Gildfind, D Smith, PA Jacobs, R Kelly, A Lefevre… - AIAA journal, 2021 - arc.aiaa.org
This paper explores the operating envelope for the University of Queensland's free-piston
driven X2 expansion tube to determine if flow conditions can be produced that generate a …

Effect of plasma sheaths on earth re-entry MHD processes

B Parent, PT Rajendran, RW Moses… - AIAA SCITECH 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-0980. vid The first study of the full
coupling between the aerothermodynamics, the magnetohydrodynamics, and the plasma …

Flow characteristics in the water-cooled channel of the MHD accelerator

DS Baranov, VA Bityurin, AN Bocharov… - Journal of Physics …, 2018 - iopscience.iop.org
Many problems related with the development of a hypersonic vehicle and development of
new thermal protection materials are directly related to the possibility of conducting a wide …

Measurement of heat-flux for magneto-aerodynamic interaction studies in a hypersonic flow

A Kkn, K Reddy - 47th AIAA Plasmadynamics and Lasers Conference, 2016 - arc.aiaa.org
I. Introduction erodynamic heating is one of the major issues in the design of planetary
atmospheric entry vehicles. Various thermal protection systems have been investigated by …

Excitation of the lowest CO2 vibrational states by electrons in hypersonic boundary layers

I Armenise - Chemical Physics, 2017 - Elsevier
The state-to-state vibrational kinetics of a CO 2/O 2/CO/C/O/e− mixture in a hypersonic
boundary layer under conditions compatible with the Mars re-entry is studied. The model …

[PDF][PDF] Radiative aerothermodynamics of entering space vehicles: toward the use of state-to-state approach

S Surzhikov, P Reynier, G Seller… - Open Plasma Phys …, 2014 - researchgate.net
Radiative Aerothermodynamics of Entering Space Vehicles: Toward the Use of State-to-State
Approach Page 1 Send Orders for Reprints to reprints@benthamscience.net The Open Plasma …

Different approximation levels in using CFD for the design of hypersonic vehicles

A Schettino, D D'Ambrosio - The Open Plasma Physics Journal, 2014 - benthamopen.com
In this paper the importance of using accurate CFD simulations in the design of hypersonic
vehicles is stressed. The attention is focused on the one hand on the need to providing the …