Add to ORKGThe purpose of this report is to release the data from the NASA Langley/Lewis 14 by 22 foot wind tunnel test that examined icing effects on a 1/8 scale twin-engine short-haul jet transport model. Presented in this document are summary data from the major configurations tested. The entire test database in addition to ice shape and model measurements is available as a data supplement in CD-ROM form. Data measured and presented are: wing pressure distributions, model force and moment, and wing surface flow visualization
A two-phase wind tunnel test was conducted in the 6 by 9 foot Icing Research Tunnel (IRT) at NASA Le...
A research project is underway at NASA Glenn to produce computer software that can accurately predic...
This report presents results from the first icing tests performed in the Modem Airfoils program. Two...
A series of wind tunnel tests were conducted to assess the effects of leading edge ice contamination...
The purpose of this report is to release the data from the NASA Langley/Lewis 14 by 22 foot wind tun...
This report documents the data collected during the large wind tunnel campaigns conducted as part of...
An experimental research effort was begun to develop a database of airplane aerodynamic characterist...
As part of NASA's Aviation Safety Program goals to reduce aviation accidents due to icing, NASA Glen...
The design and certification of modern transport airplanes for flight in icing conditions increasing...
NASA is developing and validating technology to incorporate aircraft icing effects into a flight tra...
Artificial ice shapes of various geometric fidelity were tested on a wing model based on the Common ...
Ice contaminated tailplane stall (ICTS) has been found to be responsible for 16 accidents with 139 f...
The Icing Branch at the NASA Glenn Research Center at Lewis Field initiated and conducted the Modern...
Preliminary results from the heavily instrumented ALF502R-5 engine test conducted in the NASA Glenn ...
254 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 2009.Determining the aerodynamic e...
A two-phase wind tunnel test was conducted in the 6 by 9 foot Icing Research Tunnel (IRT) at NASA Le...
A research project is underway at NASA Glenn to produce computer software that can accurately predic...
This report presents results from the first icing tests performed in the Modem Airfoils program. Two...
A series of wind tunnel tests were conducted to assess the effects of leading edge ice contamination...
The purpose of this report is to release the data from the NASA Langley/Lewis 14 by 22 foot wind tun...
This report documents the data collected during the large wind tunnel campaigns conducted as part of...
An experimental research effort was begun to develop a database of airplane aerodynamic characterist...
As part of NASA's Aviation Safety Program goals to reduce aviation accidents due to icing, NASA Glen...
The design and certification of modern transport airplanes for flight in icing conditions increasing...
NASA is developing and validating technology to incorporate aircraft icing effects into a flight tra...
Artificial ice shapes of various geometric fidelity were tested on a wing model based on the Common ...
Ice contaminated tailplane stall (ICTS) has been found to be responsible for 16 accidents with 139 f...
The Icing Branch at the NASA Glenn Research Center at Lewis Field initiated and conducted the Modern...
Preliminary results from the heavily instrumented ALF502R-5 engine test conducted in the NASA Glenn ...
254 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 2009.Determining the aerodynamic e...
A two-phase wind tunnel test was conducted in the 6 by 9 foot Icing Research Tunnel (IRT) at NASA Le...
A research project is underway at NASA Glenn to produce computer software that can accurately predic...
This report presents results from the first icing tests performed in the Modem Airfoils program. Two...