Abstract. This paper analyzes different techniques for the calibration of force balances for use in short-duration impulse hypersonic facilities such as shock tunnels. The background to how deconvolution can be used to infer aerodynamic forces on models in impulse hypersonic wind tunnels is presented along with the theory behind the different calibration techniques. Four calibration techniques are applied to a single-component stress-wave force balance. Experiments in the T4 shock tunnel using the balance demonstrate the suitability of the different calibrations for force measurements in an impulse facility. Cross checks between the calibration techniques are used to check their ranges of validity. It is shown that the impulse response deri...
A combination of modelling and analysis techniques was used to design a six component force balance....
Force tests were conducted at the long-duration-test shock tunnel JF12, which has been designed and ...
The stress-wave force balance, which was developed in the T4 facility, was tested in the HEG shock t...
This paper analyzes different techniques for the calibration of force balances for use in short-dura...
This report describes different techniques for the calibration of stress-wave force balances. A shor...
This paper presents the measurement of side force, pitching, and yawing moments on a model, using an...
Two force balance techniques for use in hypersonic impulse facilities are compared by measuring the ...
An accelerometer-based force balance was designed and developed for the measurement of drag, lift, a...
A new multiple component stress wave force balance has been designed, calibrated and tested in the H...
A new free floating internally mountable balance system that ensures unrestrained motion of the mode...
Shock tunnels are important ground test facilities that can generate high-enthalpy flow. Flight velo...
Force tests were conducted at the long-duration-test shock tunnel JF12, which has been designed and ...
Three force measurement techniques in a shock tunnel, the free-flight, movable-support force balance...
A new technique is described for measuring drag with 100-/*s rise time on a nonlifting model in a fr...
Shock tunnels create very high temperature and pressure in the nozzle plenum and flight velocities u...
A combination of modelling and analysis techniques was used to design a six component force balance....
Force tests were conducted at the long-duration-test shock tunnel JF12, which has been designed and ...
The stress-wave force balance, which was developed in the T4 facility, was tested in the HEG shock t...
This paper analyzes different techniques for the calibration of force balances for use in short-dura...
This report describes different techniques for the calibration of stress-wave force balances. A shor...
This paper presents the measurement of side force, pitching, and yawing moments on a model, using an...
Two force balance techniques for use in hypersonic impulse facilities are compared by measuring the ...
An accelerometer-based force balance was designed and developed for the measurement of drag, lift, a...
A new multiple component stress wave force balance has been designed, calibrated and tested in the H...
A new free floating internally mountable balance system that ensures unrestrained motion of the mode...
Shock tunnels are important ground test facilities that can generate high-enthalpy flow. Flight velo...
Force tests were conducted at the long-duration-test shock tunnel JF12, which has been designed and ...
Three force measurement techniques in a shock tunnel, the free-flight, movable-support force balance...
A new technique is described for measuring drag with 100-/*s rise time on a nonlifting model in a fr...
Shock tunnels create very high temperature and pressure in the nozzle plenum and flight velocities u...
A combination of modelling and analysis techniques was used to design a six component force balance....
Force tests were conducted at the long-duration-test shock tunnel JF12, which has been designed and ...
The stress-wave force balance, which was developed in the T4 facility, was tested in the HEG shock t...