A compilation of lectures presented at various Universities over a span of several years is discussed. A central theme of these lectures has been to present the research facility in terms of the service it provides to, and its potential effect on, the entire community, rather than just the research community. This theme is preserved in this paper which deals with the cryogenic transonic wind tunnels at Langley Research Center. Transonic aerodynamics is a focus both because of its crucial role in determining the success of aeronautical systems and because cryogenic wind tunnels are especially applicable to the transonics problem. The paper also provides historical perspective and technical background for cryogenic tunnels, culminating in a b...
A Boeing TR77 airfoil associated with the Advanced Technology Airfoil Test (ATAT) program was tested...
Proceedings of a conference on the cryogenic technology developed in support of a transonic wind tun...
Based on theoretical studies and experience with a low speed cryogenic tunnel and with a 1/3-meter t...
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
The characteristics and behavior of a 0.3m transonic cryogenic wind tunnel are discussed. The wide b...
A pilot transonic cryogenic pressure tunnel has recently been developed and proof tested at the NASA...
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are prese...
The theory and advantages of the cryogenic tunnel concept are briefly reviewed. The unique ability t...
The principal motivating factor was the National Transonic Facility (NTF). Since the NTF can achieve...
Fundamental aerodynamic questions for which high Reynolds number experimental capability is required...
Experiments performed at the NASA Langley Research Center in a cryogenic low-speed continuous-flow t...
A wind tunnel investigation of an advanced-technology airfoil was conducted in the Langley 0.3-Meter...
A representative, control compatible, mathematical model of a cryogenic wind tunnel was synthesized ...
The past 6 years of operation with the NASA Langley 0.3 m transonic cryogenic tunnel (TCT) show that...
A wind tunnel investigation of an advanced technology airfoil, the CAST 10-2/DOA 2, was conducted in...
A Boeing TR77 airfoil associated with the Advanced Technology Airfoil Test (ATAT) program was tested...
Proceedings of a conference on the cryogenic technology developed in support of a transonic wind tun...
Based on theoretical studies and experience with a low speed cryogenic tunnel and with a 1/3-meter t...
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
The characteristics and behavior of a 0.3m transonic cryogenic wind tunnel are discussed. The wide b...
A pilot transonic cryogenic pressure tunnel has recently been developed and proof tested at the NASA...
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are prese...
The theory and advantages of the cryogenic tunnel concept are briefly reviewed. The unique ability t...
The principal motivating factor was the National Transonic Facility (NTF). Since the NTF can achieve...
Fundamental aerodynamic questions for which high Reynolds number experimental capability is required...
Experiments performed at the NASA Langley Research Center in a cryogenic low-speed continuous-flow t...
A wind tunnel investigation of an advanced-technology airfoil was conducted in the Langley 0.3-Meter...
A representative, control compatible, mathematical model of a cryogenic wind tunnel was synthesized ...
The past 6 years of operation with the NASA Langley 0.3 m transonic cryogenic tunnel (TCT) show that...
A wind tunnel investigation of an advanced technology airfoil, the CAST 10-2/DOA 2, was conducted in...
A Boeing TR77 airfoil associated with the Advanced Technology Airfoil Test (ATAT) program was tested...
Proceedings of a conference on the cryogenic technology developed in support of a transonic wind tun...
Based on theoretical studies and experience with a low speed cryogenic tunnel and with a 1/3-meter t...