An investigation of a thermal ice-prevention system for a C-46 cargo airplane. : 7 - Effect of the thermal system on the wing-structure stresses as established in flight / by Alun R. Jones and Bernard A. Schlaff.
As part of a comprehensive investigation of a thermal ice-prevention system for a Curtiss-Wright C-46 airplane, the change in stress at various locations in the wing outer panel caused by operation of the thermal system has been determined in flight.
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| Corporate Authors: | , |
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| Other title: | NACA Wartime Reports. Series A. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1945]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. A48. |
| Subjects: |
| Summary: | As part of a comprehensive investigation of a thermal ice-prevention system for a Curtiss-Wright C-46 airplane, the change in stress at various locations in the wing outer panel caused by operation of the thermal system has been determined in flight. |
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| Item Description: | NACA Wartime Report A-48. Originally issued as NACA as Advance Restricted Report 5G20 (September 1945) Prepared at the Ames Aeronautical Laboratory, Moffett Field, California. |
| Physical Description: | 27 pages, 16 unnumbered pages : illustrations ; 27 cm. |
| Bibliography: | Includes bibliographical references. |