An investigation of aircraft heaters. : VIII - A simplified method for the calculation of the unit thermal conductance over wings / by R.C. Martinelli [and others]
A simplified approximate method of calculating the unit thermal conductance along an airfoil as a function of distance from the leading edge, by use of heat transfer data for smooth cylinders and smooth flat plates, is presented. Heat transfer rates experimentally obtained by several investigators o...
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Corporate Authors: | , |
Other title: | NACA Wartime Reports. Series W. |
Format: | Government Document Book |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1943]
|
Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. W14. |
Subjects: |
MARC
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088 | |a NACA WR W14 | ||
100 | 1 | |a Martinelli, R. C. | |
245 | 1 | 3 | |a An investigation of aircraft heaters. : |b VIII - A simplified method for the calculation of the unit thermal conductance over wings / |c by R.C. Martinelli [and others] |
246 | 3 | |a NACA Wartime Reports. Series W. | |
260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1943] | ||
300 | |a 16 pages, 10 unnumbered pages : |b illustrations ; |c 27 cm. | ||
336 | |a text |b txt |2 rdacontent. | ||
337 | |a unmediated |b n |2 rdamedia. | ||
338 | |a volume |b nc |2 rdacarrier. | ||
490 | 1 | |a Wartime Report / National Advisory Committee for Aeronautics ; |v no. W14. | |
500 | |a NACA Wartime Report W-14. | ||
500 | |a Other authors include: A.G. Guibert, E.H. Morrin, L.M.K. Boelter. | ||
500 | |a Originally issued as NACA as an Advance Restricted Report (March 1943) | ||
500 | |a Prepared at the Ames Aeronautical Laboratory, Moffett Field, California. | ||
504 | |a Includes bibliographical references. | ||
520 | 3 | |a A simplified approximate method of calculating the unit thermal conductance along an airfoil as a function of distance from the leading edge, by use of heat transfer data for smooth cylinders and smooth flat plates, is presented. Heat transfer rates experimentally obtained by several investigators on models of airfoils of sections R.A.F. 26, R.A.F. 30, Clark Y, and NACA M-6 are compared with results predicted by the use of this method. Calculations of the heat transfer rates to be expected from a typical full-scale wing are also expected. | |
650 | 0 | |a Airplanes |x Heating. | |
650 | 0 | |a Aerofoils. |0 http://id.loc.gov/authorities/subjects/sh85001301. | |
650 | 0 | |a Boundary layer. |0 http://id.loc.gov/authorities/subjects/sh85016095. | |
650 | 0 | |a Heat |x Transmission. |0 http://id.loc.gov/authorities/subjects/sh85059767. | |
650 | 0 | |a Thermal conductivity. |0 http://id.loc.gov/authorities/subjects/sh2003011072. | |
650 | 0 | |a Airplanes |x Ice prevention. |0 http://id.loc.gov/authorities/subjects/sh85002828. | |
650 | 0 | |a Mathematics. |0 http://id.loc.gov/authorities/subjects/sh85082139. | |
650 | 0 | |a Charts, diagrams, etc. |0 http://id.loc.gov/authorities/subjects/sh87002373. | |
710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. |0 http://id.loc.gov/authorities/names/n79060141 |1 http://isni.org/isni/0000000106642010. | |
710 | 2 | |a Ames Research Center. |0 http://id.loc.gov/authorities/names/n79138699 |1 http://isni.org/isni/0000000119557990. | |
830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. W14. | |
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907 | |a .b99259710 |b 11-20-17 |c 11-20-17 | ||
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952 | f | f | |p Can circulate |a University of Colorado Boulder |b Boulder Campus |c Norlin |d Norlin Library - Basement - Government Information - US |e Y 3.N 21/5:11/W-14 |h Superintendent of Documents classification |i document |m U183073231175 |n 1 |