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Development and Application of HEATED WINGS
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Language:
English
Abstract
THIS report, a discussion of the design problems in heated surface anti-icing equipment, consolidates and compiles all of the heat transfer data known to be available from past experimentation and considered to be required for current and future designs.
Consequently, the author believes that the discussion contained herein will be of assistance in some degree to designers and engineers confronted with problems relating to heated surface anti-icing.
The report deals with a rapid means of calculating heated wing requirements, charts of heat transfer coefficients, a discussion of instrumentation techniques, and a method of calculating surface temperatures in dry air.
Authors
Citation
TRIBUS, M., "Development and Application of HEATED WINGS," SAE Technical Paper 460217, 1946, https://doi.org/10.4271/460217.Also In
References
- April 1941 “Preliminary Report on Flight Tests on Airplane Having Exhaust-Heated Wings,” Rodert L. A. and others A report on the design of the exhaust-heated Lockheed 12A
- July 1941 “Flight Investigation of Thermal Properties of Exhaust-Heated Wing-De-icing System on Lockheed 12A Airplane,” Rodert L. A. and others
- NACA ARR Supplement No. 1 to above report July 1941
- NACA ARR Supplement No. 2 to above reports September 1941
- January 1942 “Recent Flight Research on Ice Prevention,” Rodert L. A. and others
- April 1942 “Preliminary Investigation and Design of Air-heated Wing for Lockheed 12A Airplane,” Rodert L. A. and others
- October 1942, to 1945 “Investigation of Aircraft Heaters,” Boelter L. M. K. and others
- February 1943 “Development of Thermal Ice Prevention Equipment for B-24D Airplane,” Rodert L. A. and others
- “Tests of Heated Low-Drag Airfoil.”
- NACA ACR December 1942 “Method for Determining Rate of Heat Transfer from Wing of Streamline Body,” Frick C. W. McCullough G. B.
- NACA Restricted Bulletin December 1942 “Method for Calculating Heat Transfer in Laminar Flow Region of Bodies,” Allen H. J. Look B. C.
- NACA Technical Memorandum No. 1045 May 1943 “Heat Transfer to Plate in Flow at High Speed,” Eckert E. Drewitz O.
- NACA Technical Memorandum No. 1044 April 1943 “Heat Transfer of Airfoils and Plates,” Seibert O.
- NACA Technical Memorandum No. 1027 August 1942 “Formation of Ice on Aircraft,” Bleeker W.
- NACA Technical Memorandum No. 1028 September 1942 “Icing of Aircraft,” Robitzsch M.
- NACA Technical Memorandum No. 1000 December 1941 “Temperature of Unheated Bodies in High-Speed Gas Stream,” Eckert E. Weise W.
- May 8 1943 “Flight Tests of Thermal Ice Prevention Equipment on Lockheed 12A Airplane,” Rodert L. A. and others
- NACA reprint of RAE Technical Note No. Inst. 674 June 1942 “Note on Kinetic Heating with Particular Reference to Conditions of Icing.”
- NACA reprint of RAE Report No. Aero 1783 November 1942 “Heat Transfer Calculations for Aerofoils,” Squire H. B.