Design and fabrication cost drivers for cryogenic transonic wind tunnel models are defined. The major cost factors for wind tunnel models are model complexity, tolerances, surface finishes, materials, material validation, and model inspection. The cryogenic temperatures require the use of materials with relatively high fracture toughness but at the same time high strength. Some of these materials are very difficult to machine, requiring extensive machine hours which can add significantly to the manufacturing costs. Some additional engineering costs are incurred to certify the materials through mechanical tests and nondestructive evaluation techniques, which are not normally required with conventional models. When instrumentation such as acc...
Thermal and stress analyses, elastic math models, verification testing, deformation and aeroelastic ...
Viewing problems associated with the measurement of model deformation in cryogenic wind tunnels are ...
The effect of thermal and caloric imperfections in cryogenic nitrogen on boundary layers was determi...
The principal motivating factor was the National Transonic Facility (NTF). Since the NTF can achieve...
The problems confronting the designer of models for cryogenic wind tunnel models are discussed with ...
Different engineering problems associated with the design of mechanisms and systems to operate in a ...
Various filler materials are being investigated for applicability to cryogenic wind tunnel models. T...
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are prese...
Interrelated research and development activities, phased development of stepped specimen program are...
As part of a NASA/DFVLR cooperation program two transonic airfoils were tested in the NASA Langley 0...
A study was undertaken to model the cryogenic wind tunnel process, to validate the model by the use ...
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
A representative, control compatible, mathematical model of a cryogenic wind tunnel was synthesized ...
Two instrumented horizontal stabilizers and one instrumented vertical stabilizer were designed and f...
The National Transonic Facility (NTF) was operational in a combined checkout and test mode for about...
Thermal and stress analyses, elastic math models, verification testing, deformation and aeroelastic ...
Viewing problems associated with the measurement of model deformation in cryogenic wind tunnels are ...
The effect of thermal and caloric imperfections in cryogenic nitrogen on boundary layers was determi...
The principal motivating factor was the National Transonic Facility (NTF). Since the NTF can achieve...
The problems confronting the designer of models for cryogenic wind tunnel models are discussed with ...
Different engineering problems associated with the design of mechanisms and systems to operate in a ...
Various filler materials are being investigated for applicability to cryogenic wind tunnel models. T...
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are prese...
Interrelated research and development activities, phased development of stepped specimen program are...
As part of a NASA/DFVLR cooperation program two transonic airfoils were tested in the NASA Langley 0...
A study was undertaken to model the cryogenic wind tunnel process, to validate the model by the use ...
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
A representative, control compatible, mathematical model of a cryogenic wind tunnel was synthesized ...
Two instrumented horizontal stabilizers and one instrumented vertical stabilizer were designed and f...
The National Transonic Facility (NTF) was operational in a combined checkout and test mode for about...
Thermal and stress analyses, elastic math models, verification testing, deformation and aeroelastic ...
Viewing problems associated with the measurement of model deformation in cryogenic wind tunnels are ...
The effect of thermal and caloric imperfections in cryogenic nitrogen on boundary layers was determi...