Study on the Similarity Criteria of Aircraft Structure Temperature/Stress/Dynamic Response
Journal of Thermal Science and Technology, 2012 The performance parameters of thermal protection system are essential for the design and optimization of high-speed aircraft. The flight-ground conversion is a valid method to provide the effective support to the design of the thermal protection ...
Lei LIU +4 more
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Inviscid design of hypersonic wind tunnel nozzles for a real gas [PDF]
, 2000 Jana Korte
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Simultaneous global pressure and temperature measurement technique for hypersonic wind tunnels [PDF]
, 2000 Gregory M. Buck
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A Review of Flow Control Strategies for Supersonic/Hypersonic Fluid Dynamics
Aerospace Research CommunicationsSupersonic and hypersonic flows have gained considerable attention in the aerospace industry in recent years. Flow control is crucial for refining the quality of these high-speed flows and improving the performance and safety of fast aircraft. This paper
Shibo Lee +9 more
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Synchronous Surface Pressure and Velocity Measurements of standard model in hypersonic flow
MATEC Web of Conferences, 2018 Experiments in the Hypersonic Wind tunnel of NUAA(NHW) present synchronous measurements of bow shockwave and surface pressure of a standard blunt rotary model (AGARD HB-2), which was carried out in order to measure the Mach-5-flow above a blunt body by ...
Zhijun Sun +4 more
doaj +1 more source
Non-isentropic effects on the WRDC 20 inch hypersonic wind tunnel calibration [PDF]
, 2003 Melvin L. Buck, Alfred C. Draper
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Ceramic and Coating Applications in the Hostile Environment of a High-Temperature Hypersonic Wind Tunnel [PDF]
, 2008 Richard L. Puster +3 more
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Boundary Layer Correction of Hypersonic Wind-tunnel Nozzle Designed by the Methods of Characteristics [PDF]
, 2014 So-Yeon Kim +4 more
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Laser-Induced Damage Features and Flow Interference of Coating Materials in Ma=6 Airflows
气体物理Aimed at the new application scenario of laser, a test platform was established to study the coating material da-mage features induced by the interaction of the Ma=6 tangential air flow and the continuous laser irradiation.
Jian LIN +6 more
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Novel heat flux controlled surface cooling for hypersonic flight. [PDF]
Sci Rep, 2023 Hufgard F +3 more
europepmc +1 more source