Results 21 to 30 of about 81,739 (264)
Research Progress of hypersonic boundary layer transition control experiments
Hypersonic boundary layer transition is a hot yet challenging problem restricting the development and breakthrough of hypersonic aerodynamics. In recent years, despite great progress made by wind tunnel experiment, transition mechanism and transition ...
He-sen Yang +6 more
doaj +1 more source
Research Progress and Prospect of Thermal Flutter of Hypersonic Vehicles
Hypersonic vehicle is subjected to severe aerodynamic load and aerodynamic heating during the flight.Thus structural dynamic stability and response caused by aerodynamic force and aerodynamic heating should be fully considered in the design process of ...
CHEN Haoyu +3 more
doaj +1 more source
Numerical Simulation of Aerodynamic Heating and Its Ground Test Simulation Technology [PDF]
Numerical simulation and related experimental research on supersonic aerodynamic heating are important contents in the development of hypersonic vehicles.
Sun Dechuan, Li Shuyue
doaj +1 more source
Polymer‐Derived High‐Temperature Nonoxide Materials: A Review
This review focuses on an attractive class of polymer‐derived high‐temperature nonoxide materials. The important parameters related to polycarbosilane pyrolysis are explained. Also, polymer‐derived solid‐solution carbides, transition metal carbides, transition metal borides, nitrides, and high‐temperature nonoxide composites are examined.
Yue Zhou, Kathy Lu
wiley +1 more source
Abstract Emissivity as a function of wavelength, direction, and temperature correlates to a material's efficiency in radiating thermal energy. Knowledge of emissivity is essential for designing and developing radiation‐cooled thermal protective systems for hypersonic applications.
Abdullah A. Saad +2 more
wiley +1 more source
Noise level effect on the hypersonic boundary layer
The boundary layer state has a critical effect on hypersonic vehicle performance and the noise level is the main factor causing the differences between the boundary layer transition in a wind tunnel test and that in a real flight.
Xinguo Sha +4 more
doaj +1 more source
This study investigated the thermal protection performance of an active jet thermal protection system (PRsAJ‐TPS) based on a new jet design parameter PRs for hypersonic flight vehicles (HFVs). The new parameter PRs is defined as the relationship between the jet flow total pressure and the free flow total pressure behind the outer bow shock.
Songyan Tian +3 more
wiley +1 more source
This paper is aimed at investigating the microstructure evolution of resin‐based ablative materials under aerodynamic heating. The microstructure, morphology, material density, and thermophysical parameters at different positions of the material after aerodynamic heating were deeply studied.
Junjie Gao +4 more
wiley +1 more source
(1) We firstly investigate the accuracy and efficiency of the high‐order discontinuous Galerkin spectral element method for the implicit large eddy simulation in oblique shock‐wave/turbulent boundary‐layer interaction. (2) We propose a new idea of improving the shock‐capturing capability of the classic Jameson shock indicator by employing a spatial ...
Min Gao +2 more
wiley +1 more source
Since the beginning of the Mars planet exploration, the characterization of carbon dioxide hypersonic flows to simulate a spaceship’s Mars atmosphere entry conditions has been an important issue.
Raphäel Vallon +5 more
doaj +1 more source

