Results 91 to 100 of about 29,751 (218)
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
core +3 more sources
Ramjet Compression System for a Hypersonic Air Transportation Vehicle Combined Cycle Engine
Energies, 2018 This report assesses the performance characteristics of a ramjet compression system in the application of a hypersonic vehicle. The vehicle is required to be self-powered and perform a complete flight profile using a combination of turbojet, ramjet and ...
Sasha Veeran +2 more
doaj +1 more source
Synthesis of Dual Phase High Entropy Ultra‐High Temperature Ceramics From Different Carbon Sources
International Journal of Applied Ceramic Technology, Volume 23, Issue 5, October 2026.ABSTRACT Dual phase (Hf,Nb,Ta,Ti,Zr)C‐(Hf,Nb,Ta,Ti,Zr)B2 ceramics were synthesized by boro‐carbothermal reduction of oxides with different carbon black powders. The starting materials reacted differently based on the particle size, surface area, and additives in the carbon powder.
Rubia Hassan +2 more
wiley +1 more source
Journal of the American Ceramic Society, Volume 109, Issue 10, October 2026.Using computational methods, we tested a common, experimentally inspired hypothesis that some secondary metals induce cubic crystal growth in Group IVB and VB transition‐metal carbides (TMCs) by becoming surface alloys that change surface energetics.
Yuchen Huang +3 more
wiley +1 more source
Data files for the article "Engineering nanoscale hypersonic phonon transport"
, 2022 Data files for the article "Engineering nanoscale hypersonic phonon transport".
J. Gomis-Bresco +15 more
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Quasiclassical trajectory computations of elementary processes in air hypersonic flows
, 2017 Collision processes of heavy particles: Quasiclassical trajectory computations of elementary processes in air hypersonic ...
Esposito, Fabrizio
core
Transpiration Cooling Tests of Porous CMC in Hypersonic Flow [PDF]
, 2011 During hypersonic flight the temperatures on the vehicle can reach very high values in certain locations. A hypersonic flight vehicle needs to be designed aerodynamically efficient. That results in rather small nose and leading edge radii which drives up
Ali Gülhan +11 more
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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
doaj +1 more source
TUSQ hypersonic wind tunnel storage
The hypersonic wind tunnel facility at the University of Southern Queensland 'TUSQ' is used in a wide variety of national and international research projects on the aerodynamics and heat transfer on aerospace ...
Buttsworth, David
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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
doaj +1 more source