Flow Field Reconstruction of 2D Hypersonic Inlets Based on a Variational Autoencoder
The inlet is one of the most important components of a hypersonic vehicle. The design and optimization of the hypersonic inlet is of great significance to the research and development of hypersonic vehicles.
Zuwei Tan, Runze Li, Yufei Zhang
doaj +3 more sources
3D Numerical Simulation and Structural Optimization for a MEMS Skin Friction Sensor in Hypersonic Flow [PDF]
The skin friction of a hypersonic vehicle surface can account for up to 50% of the total resistance, directly affecting the vehicle’s effective range and load.
Huihui Guo +4 more
doaj +2 more sources
Viscous equilibrium analysis of heat transfer on blunted cone at hypersonic flow
High speed flow requires consideration of some complex phenomena such as chemical reactions. In fact, as flow velocity increase, high temperature of hypersonic velocity excites molecules to react and causes dissociation and ionization.
F. Pish +3 more
doaj +3 more sources
Research on Star Sensor Imaging Simulation Under Near-Space Hypersonic Non-Equilibrium Flow Conditions [PDF]
In order to address the difficulty in acquiring degraded images for star sensors under hypersonic conditions, this paper proposes a star sensor imaging simulation model which can effectively analyze the influence of thermochemical non-equilibrium flow on
Zhen Liao +7 more
doaj +2 more sources
Research progress on aero-optical effects of hypersonic optical window with film cooling [PDF]
In recent years, the demand for optical imaging and detection in hypersonic aircraft has been on the rise. The high-temperature and high-pressure compressed flow field near airborne optoelectronic devices creates significant interference with light ...
Shihe Yi +4 more
doaj +2 more sources
Micro-Ramps for Hypersonic Flow Control [PDF]
Shock/boundary layer interaction (SBLI) is an undesirable phenomenon, occurring in high-speed propulsion systems. The conventional method to manipulate and control SBLI is using a bleed system that involves the removal of a certain amount of mass of the ...
Konstantinos Kontis +3 more
doaj +3 more sources
Electron losses in hypersonic flows [PDF]
The first comprehensive study of electron gains and losses in hypersonic air flows including the full coupling between non-neutral plasma sheaths and quasi-neutral plasma flows is presented here. This is made possible by the use of advanced numerical methods that overcome the stiffness associated with plasma sheaths.
B. Parent +2 more
openaire +2 more sources
Shock Wave Intelligent Prediction Method for Hypersonic Vehicle
Accurate prediction of shock wave position of hypersonic aircrafts can effectively improve the accuracy and efficiency of computational fluid dynamics (CFD) simulation.
Yuan-hao ZHU +6 more
doaj +1 more source
Design of hypersonic wavecatcher intake at Mach 12 with rectangular-to-elliptical shape transition
Wavecatcher (inward-turning) intake flows, at design Mach 12, are investigated numerically, to display the effect of wall temperature on flow structures and intake performance.
Feng-Yuan Zuo, Sannu Mölder
doaj +1 more source
A Unified Asymptotic Theory of Supersonic, Transonic, and Hypersonic Far Fields
The problems of steady, inviscid, isentropic, irrotational supersonic plane flow passing a body with a small thickness ratio was solved by the linearized theory, which is a first approximation at and near the surface but fails at far fields from the body.
Lung-Jieh Yang, Chao-Kang Feng
doaj +1 more source

