Results 21 to 30 of about 81,739 (264)

Research Progress of hypersonic boundary layer transition control experiments

open access: yesAdvances in Aerodynamics, 2022
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

open access: yesHangkong gongcheng jinzhan, 2022
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]

open access: yesHangkong bingqi, 2023
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

open access: yesAdvanced Engineering Materials, Volume 25, Issue 9, May 2023., 2023
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

Radiation heat transfer during hypersonic flight: A review of emissivity measurement and enhancement approaches of ultra‐high temperature ceramics

open access: yesInternational Journal of Ceramic Engineering &Science, Volume 5, Issue 2, March 2023., 2023
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

open access: yesAdvances in Mechanical Engineering, 2023
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

Numerical Investigation on the Thermal Protection Characteristics of a New Active Jet Design Parameter for Hypersonic Flight Vehicle

open access: yesInternational Journal of Aerospace Engineering, Volume 2023, Issue 1, 2023., 2023
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

Microstructure Evolution and Multiscale Heat Transfer Characteristics of Resin‐Based Ablative Material under Aerodynamic Heating

open access: yesInternational Journal of Aerospace Engineering, Volume 2023, Issue 1, 2023., 2023
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

On the investigation of oblique shock‐wave/turbulent boundary‐layer interactions with a high‐order discontinuous Galerkin method

open access: yesInternational Journal for Numerical Methods in Fluids, Volume 94, Issue 8, Page 1331-1357, August 2022., 2022
(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

A Compact Tunable Diode Laser Absorption Spectrometer to Monitor CO2 at 2.7 µm Wavelength in Hypersonic Flows

open access: yesSensors, 2010
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

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