Add to ORKGThe development and use of a digital computer simulation of the proposed wind tunnel facility is described. The feasibility of automatic control of wind tunnel airspeed and other parameters was examined. Specifications and implementation recommendations for a computer based automatic control and monitoring system are presented
Performance data are presented for this tunnel, which has a Mach number range from 2.0 to 3.5. The t...
Two simulations, one batch and one real-time, of an aeroelastically-scaled wind-tunnel model were de...
The hardware configuration is described for the data acquisition system (DAS) which consists of an a...
The background material and operational concepts of a computer-based system for an operating wind tu...
Aeronautical applications of simulation technology at Ames Research Center are described. The larges...
The 12-Foot Pressure Wind Tunnel at Ames Research Center is being restored. A major part of the rest...
The computer-controlled data-acquisition system recently installed for use with a transonic dynamics...
Described here is an automatic control that has been used in several forms in wind tunnels at the Wa...
The 7 by 10 foot high speed tunnel performs a wide range of tests employing a variety of model insta...
In wind tunnel tests, the problems arise of determining the wall pressure distribution, calculating ...
A wind tunnel for testing model airplanes and their parts requires accurate control of the air veloc...
Computer programs for determining performance of automatic aircraft landing system in turbulenc
The design and testing of vane sets and air-exchange inlet for the 40 x 80/80 x 120-ft wind tunnel a...
A detailed description of the Langley computer program PLOTWD which plots and fairs experimental win...
A one-dimensional distributed-parameter dynamic model of a cryogenic wind tunnel was developed which...
Performance data are presented for this tunnel, which has a Mach number range from 2.0 to 3.5. The t...
Two simulations, one batch and one real-time, of an aeroelastically-scaled wind-tunnel model were de...
The hardware configuration is described for the data acquisition system (DAS) which consists of an a...
The background material and operational concepts of a computer-based system for an operating wind tu...
Aeronautical applications of simulation technology at Ames Research Center are described. The larges...
The 12-Foot Pressure Wind Tunnel at Ames Research Center is being restored. A major part of the rest...
The computer-controlled data-acquisition system recently installed for use with a transonic dynamics...
Described here is an automatic control that has been used in several forms in wind tunnels at the Wa...
The 7 by 10 foot high speed tunnel performs a wide range of tests employing a variety of model insta...
In wind tunnel tests, the problems arise of determining the wall pressure distribution, calculating ...
A wind tunnel for testing model airplanes and their parts requires accurate control of the air veloc...
Computer programs for determining performance of automatic aircraft landing system in turbulenc
The design and testing of vane sets and air-exchange inlet for the 40 x 80/80 x 120-ft wind tunnel a...
A detailed description of the Langley computer program PLOTWD which plots and fairs experimental win...
A one-dimensional distributed-parameter dynamic model of a cryogenic wind tunnel was developed which...
Performance data are presented for this tunnel, which has a Mach number range from 2.0 to 3.5. The t...
Two simulations, one batch and one real-time, of an aeroelastically-scaled wind-tunnel model were de...
The hardware configuration is described for the data acquisition system (DAS) which consists of an a...