The principal motivating factor was the National Transonic Facility (NTF). Since the NTF can achieve significantly higher Reynolds numbers at transonic speeds than other wind tunnels in the world, and will therefore occupy a unique position among ground test facilities, every effort is being made to ensure that model design and fabrication technology exists to allow researchers to take advantage of this high Reynolds number capability. Since a great deal of experience in designing and fabricating cryogenic wind tunnel models does not exist, and since the experience that does exist is scattered over a number of organizations, there is a need to bring existing experience in these areas together and share it among all interested parties. Repre...
A wind tunnel investigation of a NASA 12-percent-thick, advanced-technology supercritical airfoil wa...
A one-dimensional distributed-parameter dynamic model of a cryogenic wind tunnel was developed which...
Two instrumented horizontal stabilizers and one instrumented vertical stabilizer were designed and f...
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
A compilation of lectures presented at various Universities over a span of several years is discusse...
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are prese...
Design and fabrication cost drivers for cryogenic transonic wind tunnel models are defined. The majo...
A representative, control compatible, mathematical model of a cryogenic wind tunnel was synthesized ...
As part of a NASA/DFVLR cooperation program two transonic airfoils were tested in the NASA Langley 0...
The National Transonic Facility (NTF) is a pressurized cryogenic wind tunnel with a 2.5 m square tes...
The characteristics and behavior of a 0.3m transonic cryogenic wind tunnel are discussed. The wide b...
The National Transonic Facility (NTF) was operational in a combined checkout and test mode for about...
Different engineering problems associated with the design of mechanisms and systems to operate in a ...
Proceedings of a conference on the cryogenic technology developed in support of a transonic wind tun...
Experiments performed at the NASA Langley Research Center in a cryogenic low-speed continuous-flow t...
A wind tunnel investigation of a NASA 12-percent-thick, advanced-technology supercritical airfoil wa...
A one-dimensional distributed-parameter dynamic model of a cryogenic wind tunnel was developed which...
Two instrumented horizontal stabilizers and one instrumented vertical stabilizer were designed and f...
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
A compilation of lectures presented at various Universities over a span of several years is discusse...
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are prese...
Design and fabrication cost drivers for cryogenic transonic wind tunnel models are defined. The majo...
A representative, control compatible, mathematical model of a cryogenic wind tunnel was synthesized ...
As part of a NASA/DFVLR cooperation program two transonic airfoils were tested in the NASA Langley 0...
The National Transonic Facility (NTF) is a pressurized cryogenic wind tunnel with a 2.5 m square tes...
The characteristics and behavior of a 0.3m transonic cryogenic wind tunnel are discussed. The wide b...
The National Transonic Facility (NTF) was operational in a combined checkout and test mode for about...
Different engineering problems associated with the design of mechanisms and systems to operate in a ...
Proceedings of a conference on the cryogenic technology developed in support of a transonic wind tun...
Experiments performed at the NASA Langley Research Center in a cryogenic low-speed continuous-flow t...
A wind tunnel investigation of a NASA 12-percent-thick, advanced-technology supercritical airfoil wa...
A one-dimensional distributed-parameter dynamic model of a cryogenic wind tunnel was developed which...
Two instrumented horizontal stabilizers and one instrumented vertical stabilizer were designed and f...