The control system was developed to control, acquire and process the data from the specially designed Roll Damping Rig to measure the roll damping derivatives of aerospace vehicle models. Steady roll technique was used for these measurements in the NAL 1.2m wind tunnel. The earlier control system was configured on two separate computers, viz. one for speed control and the other for data acquisition and processing of the rolling moment data. The system required certain important parameter entries to be duplicated exactly in both the computers for synchronization\ud of speed and acquisition of the rolling moment data. Certain other data related to the speed information were needed to be transferred from one PC to the other after the\ud blowdo...
The article shows the design and construction of a drive system for the speed control of an industri...
Abstract-The wind tunnel test control is the key to the wind tunnel tests. This article Studied 0.75...
The Dynamic Wind Tunnel Simulation Conept Has Been Used\ud To Estimate The Roll Damping Derivatives ...
Active 3-axis trim of a wind tunnel model in the Arnold Engineering Development Center’s (AEDC) Aero...
The Oscillatory Motion Support (OMS), used in the German-Dutch Wind Tunnels - Low Speed Wind Tunnel ...
A Improved Control System For A Forced-Oscillation Rig For Measurement Of Pitch/Yaw Damping Derivati...
The evolution of remote controls used to position aerodynamic control surfaces on wind tunnel test a...
After proving its individual blade control (IBC) capabilities on a four-bladed rotor system in the w...
A method is described for measuring the dynamic stability derivatives of a model airplane in a wind ...
The 12-Foot Pressure Wind Tunnel at Ames Research Center is being restored. A major part of the rest...
For over half a century the NPS Aerolabʼ Low Speed Wind Tunnel located in Halligan Hall of the Nava...
An analytic study was conducted to evaluate anticipated ranges and required accuracies for onboard l...
The aerodynamic development of vehicles in wind tunnels is currently performed via a series of stati...
The design concepts of two specialized wind tunnel model support mechanisms are described. The force...
The computer-controlled data-acquisition system recently installed for use with a transonic dynamics...
The article shows the design and construction of a drive system for the speed control of an industri...
Abstract-The wind tunnel test control is the key to the wind tunnel tests. This article Studied 0.75...
The Dynamic Wind Tunnel Simulation Conept Has Been Used\ud To Estimate The Roll Damping Derivatives ...
Active 3-axis trim of a wind tunnel model in the Arnold Engineering Development Center’s (AEDC) Aero...
The Oscillatory Motion Support (OMS), used in the German-Dutch Wind Tunnels - Low Speed Wind Tunnel ...
A Improved Control System For A Forced-Oscillation Rig For Measurement Of Pitch/Yaw Damping Derivati...
The evolution of remote controls used to position aerodynamic control surfaces on wind tunnel test a...
After proving its individual blade control (IBC) capabilities on a four-bladed rotor system in the w...
A method is described for measuring the dynamic stability derivatives of a model airplane in a wind ...
The 12-Foot Pressure Wind Tunnel at Ames Research Center is being restored. A major part of the rest...
For over half a century the NPS Aerolabʼ Low Speed Wind Tunnel located in Halligan Hall of the Nava...
An analytic study was conducted to evaluate anticipated ranges and required accuracies for onboard l...
The aerodynamic development of vehicles in wind tunnels is currently performed via a series of stati...
The design concepts of two specialized wind tunnel model support mechanisms are described. The force...
The computer-controlled data-acquisition system recently installed for use with a transonic dynamics...
The article shows the design and construction of a drive system for the speed control of an industri...
Abstract-The wind tunnel test control is the key to the wind tunnel tests. This article Studied 0.75...
The Dynamic Wind Tunnel Simulation Conept Has Been Used\ud To Estimate The Roll Damping Derivatives ...