Add to ORKGThis paper reports the basic design of a new six component force balance system using miniature piezoelectric accelerometers to measure all aerodynamic forces and moments for a test model in hypersonic shock tunnel (HST2). Since the flow duration in a hypersonic shock tunnel is of the order of $1$ ms, the balance system [1] uses fast response accelerometers (PCB Piezotronics; frequency range of 1-10 kHz) for obtaining the aerodynamic data. The alance system has been used to measure the basic aerodynamic forces and moments on a missile shaped body at Mach $8$ in the IISc hypersonic shock tunnel. The experimentally measured values match well with theoretical predictions
Shock tunnels create very high temperature and pressure in the nozzle plenum and flight velocities u...
Yawing moment, pitching moment and side-force on a blunt, triangular, lifting model were measured in...
Two force balance techniques for use in hypersonic impulse facilities are compared by measuring the ...
This paper reports the basic design of a new six component force balance system using miniature piez...
A miniature three-component accelerometer balance system for measuring the fundamental aerodynamic f...
A new six-component accelerometer force balance is developed and used in the HST2 shock tunnel of In...
This paper describes the design and development of a accelerometer-based thin flat balance system for...
This paper presents the measurement of side force, pitching, and yawing moments on a model, using an...
A force balance to measure roll, lift and drag on a lifting aerodynamic body in an ultrashort-durati...
An accelerometer-based force balance was designed and developed for the measurement of drag, lift, a...
A new free floating internally mountable balance system that ensures unrestrained motion of the mode...
In order to overcome the interference of the model mounting system with the external aerodynamics of...
An aerodynamic force test was conducted in JF12 long-test-time shock tunnel. The test time of JF12 i...
Knowledge of drag force is an important design parameter in aerodynamics. Measurement of aerodynamic...
A combination of modelling and analysis techniques was used to design a six component force balance....
Shock tunnels create very high temperature and pressure in the nozzle plenum and flight velocities u...
Yawing moment, pitching moment and side-force on a blunt, triangular, lifting model were measured in...
Two force balance techniques for use in hypersonic impulse facilities are compared by measuring the ...
This paper reports the basic design of a new six component force balance system using miniature piez...
A miniature three-component accelerometer balance system for measuring the fundamental aerodynamic f...
A new six-component accelerometer force balance is developed and used in the HST2 shock tunnel of In...
This paper describes the design and development of a accelerometer-based thin flat balance system for...
This paper presents the measurement of side force, pitching, and yawing moments on a model, using an...
A force balance to measure roll, lift and drag on a lifting aerodynamic body in an ultrashort-durati...
An accelerometer-based force balance was designed and developed for the measurement of drag, lift, a...
A new free floating internally mountable balance system that ensures unrestrained motion of the mode...
In order to overcome the interference of the model mounting system with the external aerodynamics of...
An aerodynamic force test was conducted in JF12 long-test-time shock tunnel. The test time of JF12 i...
Knowledge of drag force is an important design parameter in aerodynamics. Measurement of aerodynamic...
A combination of modelling and analysis techniques was used to design a six component force balance....
Shock tunnels create very high temperature and pressure in the nozzle plenum and flight velocities u...
Yawing moment, pitching moment and side-force on a blunt, triangular, lifting model were measured in...
Two force balance techniques for use in hypersonic impulse facilities are compared by measuring the ...