Add to ORKGThe paper deals with a small icing wind tunnel realized at the Department of Aerospace and Rocket Technologies in conjunction with the aircraft icing simulation project. There are presented some results of the airfoil ice accretion prediction and various resulting ice shapes from icing wind tunnel. Appropriate consideration is given to the ice shape geometry measurement either
A multi-phase research program in the National Research Council of Canada\u2019s Altitude Icing Wind...
To determine the process of icing on the rotating machinery, an icing experiment on a rotating airfo...
Ice shape predictions for a NACA0012 airfoil and collection efficiency predictions for the Twin Otte...
Icing tests were conducted to document ice shapes formed on three different two-dimensional airfoils...
Aerodynamic wind tunnel tests were directed to consider the impacts of different ice gradual additio...
Aerodynamic wind tunnel tests were conducted to study the effects of various ice accretions on the a...
In order to study the icing mechanism and anti-icing technology, a small low-speed reflux icing wind...
be reproduced without the written permission of the copyright owner. Flying an aircraft in icing con...
The Icing Branch at the NASA Glenn Research Center at Lewis Field initiated and conducted the Modern...
Atmospheric icing is a key challenge to the operational envelope of medium-sized fixed-wing UAVs. To...
This paper is concerned with reduced scale testing of in-flight ice accretion on aircraft surfaces. ...
254 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 2009.Determining the aerodynamic e...
Determining the aerodynamic effects of ice accretion on aircraft surfaces is an important step in ai...
Tests were conducted in the Icing Research Tunnel (IRT) atthe NASA Lewis Research Center to documen ...
Accurate representation of ice accretions is important to the study and understanding of aircraft ic...
A multi-phase research program in the National Research Council of Canada\u2019s Altitude Icing Wind...
To determine the process of icing on the rotating machinery, an icing experiment on a rotating airfo...
Ice shape predictions for a NACA0012 airfoil and collection efficiency predictions for the Twin Otte...
Icing tests were conducted to document ice shapes formed on three different two-dimensional airfoils...
Aerodynamic wind tunnel tests were directed to consider the impacts of different ice gradual additio...
Aerodynamic wind tunnel tests were conducted to study the effects of various ice accretions on the a...
In order to study the icing mechanism and anti-icing technology, a small low-speed reflux icing wind...
be reproduced without the written permission of the copyright owner. Flying an aircraft in icing con...
The Icing Branch at the NASA Glenn Research Center at Lewis Field initiated and conducted the Modern...
Atmospheric icing is a key challenge to the operational envelope of medium-sized fixed-wing UAVs. To...
This paper is concerned with reduced scale testing of in-flight ice accretion on aircraft surfaces. ...
254 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 2009.Determining the aerodynamic e...
Determining the aerodynamic effects of ice accretion on aircraft surfaces is an important step in ai...
Tests were conducted in the Icing Research Tunnel (IRT) atthe NASA Lewis Research Center to documen ...
Accurate representation of ice accretions is important to the study and understanding of aircraft ic...
A multi-phase research program in the National Research Council of Canada\u2019s Altitude Icing Wind...
To determine the process of icing on the rotating machinery, an icing experiment on a rotating airfo...
Ice shape predictions for a NACA0012 airfoil and collection efficiency predictions for the Twin Otte...