The 7 by 10 foot high speed tunnel performs a wide range of tests employing a variety of model installation methods. To support the reduction of static data from this facility, a generalized wind tunnel data reduction program had been developed for use on the Langley central computer complex. The capabilities of a version of this generalized program adapted for real time use on a dedicated on-site computer are discussed. The input specifications, instructions for the console operator, and full descriptions of the algorithms are included
This paper provides an overview of a versatile software package developed for time- and frequency-do...
The computer-controlled data-acquisition system recently installed for use with a transonic dynamics...
Real time analysis of data can reduce the time involved in exploring dynamic systems. The failure of...
The background material and operational concepts of a computer-based system for an operating wind tu...
The hardware configuration is described for the data acquisition system (DAS) which consists of an a...
The Langley 14- by 22-Foot Subsonic Tunnel is used to test a large variety of aircraft and nonaircra...
The development and use of a digital computer simulation of the proposed wind tunnel facility is des...
Performance data are presented for this tunnel, which has a Mach number range from 2.0 to 3.5. The t...
A detailed description of the Langley computer program PLOTWD which plots and fairs experimental win...
In order to meet the stringent time-critical requirements for real-time man-in-the-loop flight simul...
The equations used by the 16-Foot Transonic Wind Tunnel in the data reduction programs are presented...
A combination of software and hardware for a time-sharing computer is described which allows the use...
Performance characteristics of data acquisition system for wind tunnel digital data functio
The need to reduce time and cost of running high speed (transonic & supersonic) wind tunnels and...
To respond to the need for improved data base management and analysis capabilities for wind-tunnel d...
This paper provides an overview of a versatile software package developed for time- and frequency-do...
The computer-controlled data-acquisition system recently installed for use with a transonic dynamics...
Real time analysis of data can reduce the time involved in exploring dynamic systems. The failure of...
The background material and operational concepts of a computer-based system for an operating wind tu...
The hardware configuration is described for the data acquisition system (DAS) which consists of an a...
The Langley 14- by 22-Foot Subsonic Tunnel is used to test a large variety of aircraft and nonaircra...
The development and use of a digital computer simulation of the proposed wind tunnel facility is des...
Performance data are presented for this tunnel, which has a Mach number range from 2.0 to 3.5. The t...
A detailed description of the Langley computer program PLOTWD which plots and fairs experimental win...
In order to meet the stringent time-critical requirements for real-time man-in-the-loop flight simul...
The equations used by the 16-Foot Transonic Wind Tunnel in the data reduction programs are presented...
A combination of software and hardware for a time-sharing computer is described which allows the use...
Performance characteristics of data acquisition system for wind tunnel digital data functio
The need to reduce time and cost of running high speed (transonic & supersonic) wind tunnels and...
To respond to the need for improved data base management and analysis capabilities for wind-tunnel d...
This paper provides an overview of a versatile software package developed for time- and frequency-do...
The computer-controlled data-acquisition system recently installed for use with a transonic dynamics...
Real time analysis of data can reduce the time involved in exploring dynamic systems. The failure of...