Interest in hypersonic aerodynamic braking and aerospace planes has led to the development of new high-enthalpy hypersonic test facilities. This paper describes available techniques and future developments for making measurements in these facilities. Emphasis is on instrumentation for use with short-duration flows in free-piston shock tunnels. Issues of free-stream calibration, surface measurements on models, flow visualization, laser diagnostics, and accuracy are addressed, with references made to representative experimental studies. The paper concludes with a summary of future research needs
For future hypersonic transport aircraft or space launch vehicles based on combined cycle engines, t...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Com...
Measurements of aerodynamic forces and moments in ground-based hypersonic shock tunnels are complica...
Hypersonic and high-enthalpy wind tunnels and their measurement techniques are the cornerstone of th...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Co...
At hypersonic flight the kinetic energy of the flow is large enough that high temperature effects su...
A novel multi-component force-measurement technique has been developed and implemented at the impuls...
This report is an extension to an earlier study conducted at NAL concerning the development of a fre...
Measurements of aerodynamic forces and moments in ground-based hypersonic shock tunnels are complica...
The Goettinger High Enthalpy Tunnel (HEG) is presented as a sample of an impulse facility for aeroth...
Due to the high cost and danger associated with both manned and unmanned flight testing, a large por...
The High-Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center, DLR, is one of the ma...
The working principle of free piston driven shock tunnels is discussed and an overview of typical ap...
Only a limited number of free-stream flow properties can be measured in hypersonic impulse facilitie...
In this paper, aerodynamic testing carried out with the JF12 hypervelocity shock tunnel is reported,...
For future hypersonic transport aircraft or space launch vehicles based on combined cycle engines, t...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Com...
Measurements of aerodynamic forces and moments in ground-based hypersonic shock tunnels are complica...
Hypersonic and high-enthalpy wind tunnels and their measurement techniques are the cornerstone of th...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Co...
At hypersonic flight the kinetic energy of the flow is large enough that high temperature effects su...
A novel multi-component force-measurement technique has been developed and implemented at the impuls...
This report is an extension to an earlier study conducted at NAL concerning the development of a fre...
Measurements of aerodynamic forces and moments in ground-based hypersonic shock tunnels are complica...
The Goettinger High Enthalpy Tunnel (HEG) is presented as a sample of an impulse facility for aeroth...
Due to the high cost and danger associated with both manned and unmanned flight testing, a large por...
The High-Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center, DLR, is one of the ma...
The working principle of free piston driven shock tunnels is discussed and an overview of typical ap...
Only a limited number of free-stream flow properties can be measured in hypersonic impulse facilitie...
In this paper, aerodynamic testing carried out with the JF12 hypervelocity shock tunnel is reported,...
For future hypersonic transport aircraft or space launch vehicles based on combined cycle engines, t...
In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound. Com...
Measurements of aerodynamic forces and moments in ground-based hypersonic shock tunnels are complica...