Add to ORKGNASA Langley has a small, subsonic wind tunnel in use with the 13-inch Magnetic Suspension and Balance System (MSBS). The tunnel is capable of speeds up to Mach 0.5. This report presents tunnel design and construction details. It includes flow uniformity, angularity, and velocity fluctuation data. It also compares experimental Mach number distribution data with computed results for the General Electric Streamtube Curvature Program
The vertical open-throat wind tunnel of the National Advisory Committee for Aeronautics is described...
A series of studies were conducted to determine the existing flow quality in the NASA Lewis 8 by 6 F...
Wind tunnel magnetic suspension and balance systems (MSBSs) have so far failed to find application a...
The potential of Magnetic Suspension and Balance Systems (MSBS) to improve conventional wind tunnel ...
The U.S. aeronautical industry was surveyed to determine if current and future transonic testing req...
The current status of wind tunnel magnetic suspension and balance system development is briefly revi...
This paper will briefly review previous work in wind tunnel Magnetic Suspension and Balance Systems ...
Magnetic suspension wind tunnels offer an alternative to traditional physical support methods. They ...
Design, construction, and evaluation of magnetic suspension and balance system for wind tunnel
A few specific developments that were undertaken recently to the magnetic suspension and balance sys...
The objective of phase two of a current investigation sponsored by NASA Langley Research Center is t...
A feasibility study is in progress at NASA Glenn Research Center to implement a magnetic suspension ...
The implementation of a magnetic suspension system in the NASA Glenn Research Center (GRC) 225 cm2 S...
The objectives are to experimentally confirm several advanced design concepts on the Magnetic Suspen...
Progress in the areas of eddy current computations, modelling and analysis, design optimization meth...
The vertical open-throat wind tunnel of the National Advisory Committee for Aeronautics is described...
A series of studies were conducted to determine the existing flow quality in the NASA Lewis 8 by 6 F...
Wind tunnel magnetic suspension and balance systems (MSBSs) have so far failed to find application a...
The potential of Magnetic Suspension and Balance Systems (MSBS) to improve conventional wind tunnel ...
The U.S. aeronautical industry was surveyed to determine if current and future transonic testing req...
The current status of wind tunnel magnetic suspension and balance system development is briefly revi...
This paper will briefly review previous work in wind tunnel Magnetic Suspension and Balance Systems ...
Magnetic suspension wind tunnels offer an alternative to traditional physical support methods. They ...
Design, construction, and evaluation of magnetic suspension and balance system for wind tunnel
A few specific developments that were undertaken recently to the magnetic suspension and balance sys...
The objective of phase two of a current investigation sponsored by NASA Langley Research Center is t...
A feasibility study is in progress at NASA Glenn Research Center to implement a magnetic suspension ...
The implementation of a magnetic suspension system in the NASA Glenn Research Center (GRC) 225 cm2 S...
The objectives are to experimentally confirm several advanced design concepts on the Magnetic Suspen...
Progress in the areas of eddy current computations, modelling and analysis, design optimization meth...
The vertical open-throat wind tunnel of the National Advisory Committee for Aeronautics is described...
A series of studies were conducted to determine the existing flow quality in the NASA Lewis 8 by 6 F...
Wind tunnel magnetic suspension and balance systems (MSBSs) have so far failed to find application a...