Results 91 to 100 of about 28,434 (205)
A surrogate-based flow-field prediction and optimization strategy for hypersonic thrust nozzle
AIP AdvancesThe thrust nozzle is a component that directly generates thrust, which is of great importance in the design of a hypersonic propulsion system. In this study, a surrogate-based flow-field prediction and optimization strategy for hypersonic thrust nozzles ...
Helin Huang, Qiancheng Wang, Zeping Wu
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Analysis of Aerothermal Environment Characteristics of Hypersonic Rudder Shaft Gaps
气体物理Rudder shaft gaps of hypersonic vehicles affect the flow structure and corresponding aerodynamic heating characteristics, resulting in local peak heating near the rudder shaft, which poses a safety risk to the local thermal protection system.
Zhiyi REN +4 more
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Stabilizing Hierarchical Heterostructures Enables Impact‐Resistant High‐Entropy Alloys
Rare Metals, Volume 45, Issue 9, September 2026.
Liqiang Wang, Liming Lei
wiley +1 more source
Research on Thermal Protection of Control Rudder Shaft of Hypersonic Vehicle
气体物理The control rudder is a key component for controlling the attitude of hypersonic aircraft, but the gap area of the rudder is prone to serious thermal load problems.
Jiaqi QIN, Zhiwei SHI, Weilin ZHANG
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Hypersonic Flow Theory and Hypersonic Aerodynamics [PDF]
Journal of Applied Mechanics, 1960 Wallace D. Hayes +3 more
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A study of roughness in turbulent hypersonic boundary-layers [PDF]
, 1993 The influence of large scale regular roughness on a Mach 5 turbulent boundary layer and a compression corner was investigated on axisymmetric wind tunnel models.
Babinsky, Holger
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Experimental study of slender vehicles at hypersonic speeds
, 1996 An experimental investigation of the hypersonic flow over (i) a wing-body configuration, (ii) a hemi-spherically blunted cone-cylinder body and (iii) a one-half- power-law body has been conducted for M,, = 8.2 and Re,, = 9.35x104
Singh, Amarjit
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CeramicsCeramic materials are indispensable to aerospace and defence technologies, where structural and functional components are required to withstand extreme thermal, mechanical, and chemically aggressive environments.
Alfredo Aguilar-Elguezabal +4 more
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An Open-Source Code for High-Speed Non-Equilibrium Gas–Solid Flows in OpenFOAM
AerospaceThis paper details the development and verification tests of an open-source code named hy2LPTFoam intended for solving high-speed non-equilibrium gas-particle flows in OpenFOAM.
Ziqu Cao, Xiaofeng Zhang, Yonghe Zhang
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SHEFEX-2 - Development Status of the Vehicle and Sub-Systems for a Hypersonic Re-Entry Flight Experiment [PDF]
, 2009 The SHarp Edge Flight EXperiment (SHEFEX) is a DLR program to investigate aerodynamic behaviour and thermal protection problems of re-entry vehicles at hypersonic velocities, using unconventional shapes comprising multi-facetted surfaces with sharp edges.
Turner, Peter +4 more
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