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...

Full description

Saved in:
Bibliographic Details
Main Author: Martinelli, R. C.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Ames Research Center
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

LEADER 00000cam a2200000Ia 4500
001 b9925971
003 CoU
005 20171120122430.0
008 110407s1943 dcua bt f000 0 eng d
035 |a (OCoLC)ocn711782518 
035 |a (OCoLC)711782518 
040 |a LHL  |b eng  |c LHL  |d LHL  |d OCLCO  |d FTU  |d OCLCQ  |d FTU  |d COD 
049 |a COD9 
086 0 |a Y 3.N 21/5:11/W-14 
086 0 |a Y 3.N 21/5:11/W-14 
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. 
907 |a .b99259710  |b 03-19-20  |c 11-20-17 
998 |a gov  |b 11-20-17  |c r  |d m   |e -  |f eng  |g dcu  |h 3  |i 1 
907 |a .b99259710  |b 12-01-17  |c 11-20-17 
944 |a MARS - RDA ENRICHED 
907 |a .b99259710  |b 11-20-17  |c 11-20-17 
948 |a gro17/18:cjg 
999 f f |i f8d74dbd-52e6-5e03-85a7-564d0e8c0094  |s 2b530b16-4018-5b0e-b50f-077b3d67dfea 
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