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
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
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Research on Thermal Protection of Control Rudder Shaft of Hypersonic Vehicle
气体物理The control rudder is a key component for controlling the attitude of hypersonic aircraft, but the gap area of the rudder is prone to serious thermal load problems.
Jiaqi QIN, Zhiwei SHI, Weilin ZHANG
doaj +1 more source
Analysis of Air-Breathing Hypersonic Maneuver Flight Styles and Key Technologies [PDF]
Hangkong bingqiThe maneuver flight performance is one of the key capabilities to ensure the implementation of various applications for air-breathing hypersonic aircraft.
Duan Pengfei, Gao Shuliang, Wang Enliang, Wang Han
doaj +1 more source
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
core +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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Propagation of Elastic Waves in a One-Dimensional High Aspect Ratio Nanoridge Phononic Crystal
Applied Sciences, 2018 We investigate the propagation of elastic waves in a one-dimensional (1D) phononic crystal constituted by high aspect ratio epoxy nanoridges that have been deposited at the surface of a glass substrate.
Abdellatif Gueddida +4 more
doaj +1 more source
Boron‐Intervened Reaction‐Pathway and Interface‐State Engineering for Ductile Refractory Alloys
Rare Metals, Volume 45, Issue 10, October 2026.
Jikui Liu, Bingnan Qian
wiley +1 more source
Hypersonic Flow Theory and Hypersonic Aerodynamics [PDF]
Journal of Applied Mechanics, 1960 Wallace D. Hayes +3 more
openaire +1 more source
SHEFEX-2 - Development Status of the Vehicle and Sub-Systems for a Hypersonic Re-Entry Flight Experiment [PDF]
, 2009 The SHarp Edge Flight EXperiment (SHEFEX) is a DLR program to investigate aerodynamic behaviour and thermal protection problems of re-entry vehicles at hypersonic velocities, using unconventional shapes comprising multi-facetted surfaces with sharp edges.
Turner, Peter +4 more
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