A procedure proposed for use in the design of air-heated systems for the continuous prevention of ice formation on airplane components is set forth. Required heat-transfer and air-pressure-loss equations are presented, and methods of selecting appropriate meteorological conditions for flight over specified geographical areas and for the calculation of water-drop-impingement characteristics are suggested. In order to facilitate the design, a simple electrical analogue was devised which solves the complex heat-transfer relationships existing in the thermal-system analysis. The analogue is described and an illustration of its application to design is given
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.Airc...
The heat requirements for the icing protection of two radome configurations have been studied over a...
An investigation was conducted in the NACA Lewis icing research tunnel to determine the characterist...
A procedure proposed for use in the design of air-heated systems\ud for the continuous prevention of...
Flight tests were made in natural icing conditions with two 8-ft-chord heated airfoils of different ...
The design analysis showed that the thermal requirements for the anti-icing systems of the wings, th...
The basic idea in the design of the system described was to raise the temperature of the surfaces to...
Two topics of interest to persons attempting to apply the heat method of preventing ice formation on...
This investigation was conducted to study the practicability of employing heat as a means of prevent...
Thermal ice protection systems use heat energy to prevent a dangerous buildup of ice on an aircraft....
Presented at 2018 Aviation Technology, Integration, and Operations Conference (AIAA 2018-4136)A ther...
The effects of existing frictional heating were analyzed to determine the conditions under which ice...
A method is given for calculating the temperature that a surface, heated internally by air, will ass...
The National Advisory Committee for Aeronautics has conducted exhaust-heat de-icing tests inflight t...
Meteorological conditions conducive to aircraft icing are arranged in four classifications: three ar...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.Airc...
The heat requirements for the icing protection of two radome configurations have been studied over a...
An investigation was conducted in the NACA Lewis icing research tunnel to determine the characterist...
A procedure proposed for use in the design of air-heated systems\ud for the continuous prevention of...
Flight tests were made in natural icing conditions with two 8-ft-chord heated airfoils of different ...
The design analysis showed that the thermal requirements for the anti-icing systems of the wings, th...
The basic idea in the design of the system described was to raise the temperature of the surfaces to...
Two topics of interest to persons attempting to apply the heat method of preventing ice formation on...
This investigation was conducted to study the practicability of employing heat as a means of prevent...
Thermal ice protection systems use heat energy to prevent a dangerous buildup of ice on an aircraft....
Presented at 2018 Aviation Technology, Integration, and Operations Conference (AIAA 2018-4136)A ther...
The effects of existing frictional heating were analyzed to determine the conditions under which ice...
A method is given for calculating the temperature that a surface, heated internally by air, will ass...
The National Advisory Committee for Aeronautics has conducted exhaust-heat de-icing tests inflight t...
Meteorological conditions conducive to aircraft icing are arranged in four classifications: three ar...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.Airc...
The heat requirements for the icing protection of two radome configurations have been studied over a...
An investigation was conducted in the NACA Lewis icing research tunnel to determine the characterist...