A New Hypersonic Wind Tunnel Force Measurement System to Reduce Additional Bending Moment and Avoid Time-Varying Stiffness [PDF]
In order to improve traditional hypersonic wind tunnel airframe/propulsion integrated aerodynamic testing technology for hypersonic vehicles, a new force measurement system called the aerodynamic force measuring support (AFMS) was designed.
Shichao Li+3 more
doaj +2 more sources
3D Numerical Simulation and Structural Optimization for a MEMS Skin Friction Sensor in Hypersonic Flow [PDF]
The skin friction of a hypersonic vehicle surface can account for up to 50% of the total resistance, directly affecting the vehicle’s effective range and load.
Huihui Guo+4 more
doaj +2 more sources
MEMS Skin Friction Sensor with High Response Frequency and Large Measurement Range [PDF]
Micro-electromechanical system (MEMS) skin friction sensors are considered to be promising sensors in hypersonic wind tunnel experiments owing to their miniature size, high sensitivity, and stability.
Huihui Guo+4 more
doaj +2 more sources
Micro-Assembly Error Control of Specialized MEMS Friction Sensor [PDF]
A skin friction sensor is a three-dimensional MEMS sensor specially designed for measuring the skin friction of hypersonic vehicle models. The accuracy of skin friction measurement under hypersonic laminar flow conditions is closely related to the ...
Wei Zhou+4 more
doaj +2 more sources
Hypersonic Aerodynamic Force Balance Using Micromachined All-Fiber Fabry–Pérot Interferometric Strain Gauges [PDF]
This paper presents high-sensitivity, micromachined all-fiber Fabry–Pérot interferometric (FFPI) strain gauges and their integration in a force balance for hypersonic aerodynamic measurements.
Huacheng Qiu+4 more
doaj +2 more sources
A novel method to realize a non-uniform heat flux distribution through the variable-speed scanning of an electron beam [PDF]
Quartz lamp heaters and hypersonic wind tunnel are currently applied in thermal assessment of heat resistant materials and surface of aircraft. However, it is difficult to achieve precise heat flux distribution by quartz lamp heaters, while enormous ...
Chuanmao Zheng+3 more
doaj +2 more sources
Fabrication and Hypersonic Wind Tunnel Validation of a MEMS Skin Friction Sensor Based on Visual Alignment Technology. [PDF]
Wang X, Wang N, Xu X, Zhu T, Gao Y.
europepmc +3 more sources
New Transonic Tests of HB-2 Hypersonic Standard Models in the VTI T-38 Trisonic Wind Tunnel
Recent experience has shown that test results of standard wind tunnel models under off-design conditions could be a useful aid in preparations of some nonstandard wind tunnel tests.
Dijana Damljanović+3 more
doaj +2 more sources
Characterization of Freestream Disturbances in Conventional Hypersonic Wind Tunnels. [PDF]
Duan L+13 more
europepmc +2 more sources
Direct Numerical Simulation of Acoustic Noise Generation from the Nozzle Wall of a Hypersonic Wind Tunnel [PDF]
Junji Huang, L. Duan
semanticscholar +2 more sources