The problems confronting the designer of models for cryogenic wind tunnel models are discussed with particular reference to the difficulties in obtaining appropriate data on the mechanical and physical properties of candidate materials and their fabrication technologies. The relationship between strength and toughness of alloys is discussed in the context of maximizing both and avoiding the problem of dimensional and microstructural instability. All major classes of materials used in model construction are considered in some detail and in the Appendix selected numerical data is given for the most relevant materials. The stepped-specimen program to investigate stress-induced dimensional changes in alloys is discussed in detail together with ...
As part of a NASA/DFVLR cooperation program two transonic airfoils were tested in the NASA Langley 0...
The criteria used to prevent failure of wind-tunnel models and support hardware were revised as par...
The development of two high Reynolds number wind tunnels at NASA Langley Research Center which opera...
Interrelated research and development activities, phased development of stepped specimen program are...
A proposed configuration for a stepped specimen to be used in the system evaluation of mechanisms th...
Various filler materials are being investigated for applicability to cryogenic wind tunnel models. T...
Design and fabrication cost drivers for cryogenic transonic wind tunnel models are defined. The majo...
The problem of dimensional instability in airfoil models for cryogenic wind tunnels is discussed in ...
This report documents the results of a dimensional stability analysis of seventeen stepped specimens...
Different engineering problems associated with the design of mechanisms and systems to operate in a ...
The principal motivating factor was the National Transonic Facility (NTF). Since the NTF can achieve...
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are prese...
The fracture resistance and fatigue response of Armco Nitronic 40 austenitic stainless steel were ev...
An overview and status of current activities seeking alternatives to 200 grade 18Ni Steel CVM alloy ...
Several different tests are described which simulated the actual configuration of a cryogenic wind t...
As part of a NASA/DFVLR cooperation program two transonic airfoils were tested in the NASA Langley 0...
The criteria used to prevent failure of wind-tunnel models and support hardware were revised as par...
The development of two high Reynolds number wind tunnels at NASA Langley Research Center which opera...
Interrelated research and development activities, phased development of stepped specimen program are...
A proposed configuration for a stepped specimen to be used in the system evaluation of mechanisms th...
Various filler materials are being investigated for applicability to cryogenic wind tunnel models. T...
Design and fabrication cost drivers for cryogenic transonic wind tunnel models are defined. The majo...
The problem of dimensional instability in airfoil models for cryogenic wind tunnels is discussed in ...
This report documents the results of a dimensional stability analysis of seventeen stepped specimens...
Different engineering problems associated with the design of mechanisms and systems to operate in a ...
The principal motivating factor was the National Transonic Facility (NTF). Since the NTF can achieve...
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are prese...
The fracture resistance and fatigue response of Armco Nitronic 40 austenitic stainless steel were ev...
An overview and status of current activities seeking alternatives to 200 grade 18Ni Steel CVM alloy ...
Several different tests are described which simulated the actual configuration of a cryogenic wind t...
As part of a NASA/DFVLR cooperation program two transonic airfoils were tested in the NASA Langley 0...
The criteria used to prevent failure of wind-tunnel models and support hardware were revised as par...
The development of two high Reynolds number wind tunnels at NASA Langley Research Center which opera...