A need has arisen for a new wind tunnel facility with unique capabilities for testing propulsion systems and for conducting research in adverse weather conditions. New propulsion system concepts, new aircraft configurations with an unprecedented degree of propulsion system/aircraft integration, and requirements for aircraft operation in adverse weather dictate the need for a new test facility. Required capabilities include simulation of both altitude pressure and temperature, large size, full subsonic speed range, propulsion system operation, and weather simulation (i.e., icing, heavy rain). A cost effective rehabilitation of the NASA Lewis Research Center's Altitude Wind Tunnel (AWT) will provide a facility with all these capabilities
Aeronautical applications of simulation technology at Ames Research Center are described. The larges...
In a closed loop icing wind tunnel the icing cloud is simulated by introducing tiny water droplets t...
The Icing Research Tunnel is used extensively to test many classes of aircraft under atmospheric ici...
Currently experimental aircraft icing research is severely hampered by limitations of ground icing s...
An effort is currently underway at the NASA Lewis Research Center to rehabilitate and extend the cap...
Efforts are currently underway at NASA Lewis to improve and expand ground test facilities and to dev...
NASA maintains twelve major wind tunnels at three field centers capable of providing flows at 0.1 M ...
Specially designed wind tunnel setups make it possible to simulate various weather hazards, in an im...
As the propulsion and power generation center of NASA, Lewis has designed its wind tunnels for propu...
Comments on films of tests simulating rain and ice conditions in a wind tunnel are presented, with t...
This report describes the results of an engineering study conducted for NASA-Lewis Research Center o...
Rehabilitation and extention of the capability of the altitude wind tunnel (AWT) was analyzed. The a...
A brief history of the 8x6 Supersonic Wind Tunnel (SWT) and 9x15 Low Speed Wind Tunnel (LSWT) at NAS...
Within the past 10 years there have been placed in operation in the United States four low-turbulenc...
It is desirable to test sportswear and sports equipment at exactly the same conditions experienced d...
Aeronautical applications of simulation technology at Ames Research Center are described. The larges...
In a closed loop icing wind tunnel the icing cloud is simulated by introducing tiny water droplets t...
The Icing Research Tunnel is used extensively to test many classes of aircraft under atmospheric ici...
Currently experimental aircraft icing research is severely hampered by limitations of ground icing s...
An effort is currently underway at the NASA Lewis Research Center to rehabilitate and extend the cap...
Efforts are currently underway at NASA Lewis to improve and expand ground test facilities and to dev...
NASA maintains twelve major wind tunnels at three field centers capable of providing flows at 0.1 M ...
Specially designed wind tunnel setups make it possible to simulate various weather hazards, in an im...
As the propulsion and power generation center of NASA, Lewis has designed its wind tunnels for propu...
Comments on films of tests simulating rain and ice conditions in a wind tunnel are presented, with t...
This report describes the results of an engineering study conducted for NASA-Lewis Research Center o...
Rehabilitation and extention of the capability of the altitude wind tunnel (AWT) was analyzed. The a...
A brief history of the 8x6 Supersonic Wind Tunnel (SWT) and 9x15 Low Speed Wind Tunnel (LSWT) at NAS...
Within the past 10 years there have been placed in operation in the United States four low-turbulenc...
It is desirable to test sportswear and sports equipment at exactly the same conditions experienced d...
Aeronautical applications of simulation technology at Ames Research Center are described. The larges...
In a closed loop icing wind tunnel the icing cloud is simulated by introducing tiny water droplets t...
The Icing Research Tunnel is used extensively to test many classes of aircraft under atmospheric ici...