Development of combined hypersonic test facility for aerothermodynamic testing. [PDF]
Yang S, Choi I, Park G.
europepmc +1 more source
High-Emissivity M<sup>2+</sup>@TiO<sub>2</sub>/High-Entropy Coating on Flexible Aluminosilicate Fiber Fabric for Enhanced Bonding Strength and Thermal Insulation Performance. [PDF]
Xu J, Zhang X, Ma X, Liu J.
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AlN-based aerogel thermo-cooler enabled by enhanced phonon conduction and unconstrained liquid capillarity. [PDF]
Meng S +5 more
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Efficient launching of shear phonons in photostrictive halide perovskites. [PDF]
Horiachyi DO +12 more
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ML for fast assimilation of wall-pressure measurements from hypersonic flow over a cone. [PDF]
Morra P, Meneveau C, Zaki TA.
europepmc +1 more source
Weak wall boundary conditions for compressible flows. [PDF]
Jaiswal M +4 more
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Research Progress on Thermal Insulation Material Systems for High-Speed Aircrafts. [PDF]
Jiang X, Guo Y, Zhou Y.
europepmc +1 more source
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Research progress on active thermal protection for hypersonic vehicles
Progress in Aerospace Sciences, 2020Hypersonic vehicles with scramjet engine as propulsion devices is one of the most important developing trends in the aerospace field for both commercial and military application. The encountered huge aerodynamic heating and strong combustion heat release
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Inertial navigation system/global navigation satellite system/celestial navigation system (INS/GNSS/CNS) integration is a favorable navigation mode for hypersonic vehicles.
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Pressure fluctuations play an essential role in the transport of turbulent kinetic energy and vibrational loading. This study focuses on examining the effect of wall cooling on pressure fluctuations in compressible turbulent boundary layers by high ...
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