The more important changes to the 0.1 m cryogenic wind tunnel since its completion in 1977 are outlined. These include detailed improvements in the fan drive to allow higher speeds, and the provision of a test section leg suitable for use with a magnetic suspension and balance system. The instrumentation, data logging, data reduction and tunnel controls were also improved and modernized. A tunnel performance summary is given
A compilation of lectures presented at various Universities over a span of several years is discusse...
This report presents part of the tests for verification of the T2 transonic induction wind tunnel in...
Different engineering problems associated with the design of mechanisms and systems to operate in a ...
The characteristics and behavior of a 0.3m transonic cryogenic wind tunnel are discussed. The wide b...
The design and performance of a low speed one atmosphere cryogenic wind tunnel is described. The tun...
A representative, control compatible, mathematical model of a cryogenic wind tunnel was synthesized ...
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are prese...
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
The goals, design, problems, and value of cryogenic transonic wind tunnels being developed in Europe...
Cold wire measurement of temperature fluctuations were made in a DERAT T'2 induction powered cryogen...
The design of a cryogenic wind tunnel which operates continuously, and is capable of attaining trans...
A one-dimensional distributed-parameter dynamic model of a cryogenic wind tunnel was developed which...
Experiments performed at the NASA Langley Research Center in a cryogenic low-speed continuous-flow t...
Based on theoretical studies and experience with a low speed cryogenic tunnel and with a 1/3-meter t...
The principal motivating factor was the National Transonic Facility (NTF). Since the NTF can achieve...
A compilation of lectures presented at various Universities over a span of several years is discusse...
This report presents part of the tests for verification of the T2 transonic induction wind tunnel in...
Different engineering problems associated with the design of mechanisms and systems to operate in a ...
The characteristics and behavior of a 0.3m transonic cryogenic wind tunnel are discussed. The wide b...
The design and performance of a low speed one atmosphere cryogenic wind tunnel is described. The tun...
A representative, control compatible, mathematical model of a cryogenic wind tunnel was synthesized ...
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are prese...
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
The goals, design, problems, and value of cryogenic transonic wind tunnels being developed in Europe...
Cold wire measurement of temperature fluctuations were made in a DERAT T'2 induction powered cryogen...
The design of a cryogenic wind tunnel which operates continuously, and is capable of attaining trans...
A one-dimensional distributed-parameter dynamic model of a cryogenic wind tunnel was developed which...
Experiments performed at the NASA Langley Research Center in a cryogenic low-speed continuous-flow t...
Based on theoretical studies and experience with a low speed cryogenic tunnel and with a 1/3-meter t...
The principal motivating factor was the National Transonic Facility (NTF). Since the NTF can achieve...
A compilation of lectures presented at various Universities over a span of several years is discusse...
This report presents part of the tests for verification of the T2 transonic induction wind tunnel in...
Different engineering problems associated with the design of mechanisms and systems to operate in a ...