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
254 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 2009.Determining the aerodynamic e...
Accurate representation of ice accretions is important to the study and understanding of aircraft ic...
Ice contaminated tailplane stall (ICTS) has been found to be responsible for 16 accidents with 139 f...
The purpose of this report is to release the data from the NASA Langley/Lewis 14 by 22 foot wind tun...
A series of wind tunnel tests were conducted to assess the effects of leading edge ice contamination...
This report documents the data collected during the large wind tunnel campaigns conducted as part of...
NASA is developing and validating technology to incorporate aircraft icing effects into a flight tra...
Aerodynamic wind tunnel tests were directed to consider the impacts of different ice gradual additio...
Icing tests were conducted to document ice shapes formed on three different two-dimensional airfoils...
An experimental research effort was begun to develop a database of airplane aerodynamic characterist...
The paper deals with a small icing wind tunnel realized at the Department of Aerospace and Rocket Te...
Aerodynamic wind tunnel tests were conducted to study the effects of various ice accretions on the a...
As part of NASA's Aviation Safety Program goals to reduce aviation accidents due to icing, NASA Glen...
This report makes use of the results obtained in the Gottingen ice tunnel in which the atmospheric c...
Wind-tunnel testing of ice accretion over aircraft wings is simulated numerically to investigate the...
254 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 2009.Determining the aerodynamic e...
Accurate representation of ice accretions is important to the study and understanding of aircraft ic...
Ice contaminated tailplane stall (ICTS) has been found to be responsible for 16 accidents with 139 f...
The purpose of this report is to release the data from the NASA Langley/Lewis 14 by 22 foot wind tun...
A series of wind tunnel tests were conducted to assess the effects of leading edge ice contamination...
This report documents the data collected during the large wind tunnel campaigns conducted as part of...
NASA is developing and validating technology to incorporate aircraft icing effects into a flight tra...
Aerodynamic wind tunnel tests were directed to consider the impacts of different ice gradual additio...
Icing tests were conducted to document ice shapes formed on three different two-dimensional airfoils...
An experimental research effort was begun to develop a database of airplane aerodynamic characterist...
The paper deals with a small icing wind tunnel realized at the Department of Aerospace and Rocket Te...
Aerodynamic wind tunnel tests were conducted to study the effects of various ice accretions on the a...
As part of NASA's Aviation Safety Program goals to reduce aviation accidents due to icing, NASA Glen...
This report makes use of the results obtained in the Gottingen ice tunnel in which the atmospheric c...
Wind-tunnel testing of ice accretion over aircraft wings is simulated numerically to investigate the...
254 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 2009.Determining the aerodynamic e...
Accurate representation of ice accretions is important to the study and understanding of aircraft ic...
Ice contaminated tailplane stall (ICTS) has been found to be responsible for 16 accidents with 139 f...