THIS paper presents the results of an internal research effort to develop and validate
instrumentation for the direct measurement of aerodynamic forces and moments on reentry …

An external force balance for a hypersonic shock tunnel was developed. The design utilized
finite element analysis that identified the dynamics of the balance. A simulated impulse and …

Experiments to measure the forces and moments acting on a blunted-cone capsule model
are conducted in the High Enthalpy Shock Tunnel Göttingen. A free-flying arrangement is …

临近空间高超声速飞行器具有速度快, 突防能力强, 杀伤力大等特点, 是当今世界各军事强国新型
武器的重点发展方向. 其中, 气动力和气动热是高超声速飞行器的两项重要指标 …

Static aerodynamic force measurement is generally of interest in both low-and high-speed
ground test facilities, but dynamic force measurement is typically associated with higher …

在高超声速风洞测力试验过程中, 冲击载荷或动态载荷激励测力系统结构振动,
天平输出信号中包含了振动干扰量, 可通过动态补偿方法进行改善, 但现有方法处理方式单一 …

Current research in hypersonic wind tunnel aerodynamic testing predominantly focuses on
small-scale and lightweight models, typically limited to scales of 4 m and weights under 1 …

A new method for input signal reconstruction is presented. This approach utilizes the
convolution relationship of inputs and outputs of linear systems. A linear discretization of …

View Video Presentation: https://doi. org/10.2514/6.2023-3712. vid Free-flight experiments
allow for the opportunity to capture the unrestricted flight of a test geometry and observe its …

A blunt double-cone model, equipped with a three-component accelerometer or piezofilm-
based force balance system, is tested in the IITB-Shock Tunnel at 0 º and 10 º angle of …