Aeronautical noise suppression at transonic Mach numbers [PDF]
The measurement of wind tunnel background pressure fluctuations in a Ludwig Tube is discussed. The measurements are to provide improved unsteady aerodynamic data for the design of aeronautical vehicles. The preliminary results of the facility calibration
Mccanless, G. F., Jr.
core +1 more source
Design of Data Acquisition System for Silicon Micro Machined Resonant Accelerometer [PDF]
Yun Xu, Yaohui Qu, Zhihang Luo
openalex +1 more source
High resolution resonant accelerometer based on MEMS technology
Xudong Zou
openalex +1 more source
W7.3.4 - Sensitivity Tuning and ON/OFF Switching in a Resonant Micro-accelerometer
A. A. Zobova +2 more
openalex +2 more sources
Structure Design of Micromechanical Silicon Resonant Accelerometer [PDF]
Libin Huang +42 more
openalex +1 more source
Structure Design Optimization of a Differential Capacitive MEMS Accelerometer Based on a Multi-Objective Elitist Genetic Algorithm. [PDF]
Yang D +10 more
europepmc +1 more source
Frequency-Comb-like Behavior in a Resonant MEMS Accelerometer Subject to Blue Sideband Excitation
Jingqian Xi +10 more
openalex +2 more sources
Design and Analysis of Silicon Resonant Accelerometer [PDF]
Jing Li, Shangchun Fan, Zhanshe Guo
openalex +1 more source
An Angle-Dependent Bias Compensation Method for Hemispherical Resonator Gyro Inertial Navigation Systems. [PDF]
Liu C +9 more
europepmc +1 more source

