A comparison of two methods for calculating transient temperatures for thick walls / James J. Buglia and Helen Brinkworth.

A comparison is made of two different methods of calculating transient temperatures for thick walls with arbitrary variation of heat-transfer coefficient and adiabatic-wall temperature. Although numerical calculations for special cases for which the exact solutions are available show that both metho...

Full description

Saved in:
Bibliographic Details
Main Author: Buglia, James J.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Brinkworth, Helen
Format: Government Document Book
Language:English
Published: Washington : National Advisory Committee for Aeronautics, [1958]
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 4343.
Subjects:

MARC

LEADER 00000cam a2200000Ia 4500
001 b9105823
003 CoU
008 101214e195808 dcua bt f000 0 eng d
005 20231211205752.8
035 |a (OCoLC)ocn692434552 
035 |a (OCoLC)692434552 
040 |a LHL  |b eng  |c LHL  |d LHL  |d OCLCF  |d OCLCO  |d OCLCQ  |d COD 
049 |a COD9 
086 0 |a Y 3.N 21/5:6/4343 
088 |a NACA TN 4343 
100 1 |a Buglia, James J.  |0 http://id.loc.gov/authorities/names/n81057961  |1 http://isni.org/isni/0000000024680689. 
245 1 2 |a A comparison of two methods for calculating transient temperatures for thick walls /  |c James J. Buglia and Helen Brinkworth. 
260 |a Washington :  |b National Advisory Committee for Aeronautics,  |c [1958] 
300 |a 19 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 Technical note / National Advisory Committee for Aeronautics ;  |v 4343. 
500 |a "August 1958." 
500 |a NACA TN Number 4343. 
504 |a Includes bibliographical references. 
520 3 |a A comparison is made of two different methods of calculating transient temperatures for thick walls with arbitrary variation of heat-transfer coefficient and adiabatic-wall temperature. Although numerical calculations for special cases for which the exact solutions are available show that both methods give satisfactory results, Hill's method (NACA Technical Note 4105) consistently gives nearly exact results with considerably less computing time, except for the case in which a temperature profile through the thick skin is desired. For this case, Dusinberre's method (Transactions, American Society of Mechanical Engineers, Volume 67, No. 8) is much faster, though less accurate. 
583 1 |a committed to retain  |c 20230101  |d 20480101  |5 CoU  |f Alliance Shared Trust  |u https://www.coalliance.org/shared-print-archiving-policies. 
650 0 |a Temperature.  |0 http://id.loc.gov/authorities/subjects/sh85133712. 
650 0 |a Heat  |x Transmission.  |0 http://id.loc.gov/authorities/subjects/sh85059767. 
650 0 |a Mathematical analysis.  |0 http://id.loc.gov/authorities/subjects/sh85082116. 
650 7 |a Heat  |x Transmission.  |2 fast  |0 (OCoLC)fst00953826. 
650 7 |a Mathematical analysis.  |2 fast  |0 (OCoLC)fst01012068. 
650 7 |a Temperature.  |2 fast  |0 (OCoLC)fst01147333. 
700 1 |a Brinkworth, Helen. 
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. 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v 4343.  |0 http://id.loc.gov/authorities/names/no2009017392. 
907 |a .b91058235  |b 08-13-20  |c 04-28-17 
998 |a pas  |b 04-28-17  |c r  |d m   |e -  |f eng  |g dcu  |h 2  |i 1 
907 |a .b91058235  |b 10-26-19  |c 04-28-17 
944 |a MARS - RDA ENRICHED 
907 |a .b91058235  |b 05-01-17  |c 04-28-17 
907 |a .b91058235  |b 04-28-17  |c 04-28-17 
948 |a gro16/17:cjg 
999 f f |i 85d94a3f-3097-51d6-9175-49ed436fb83b  |s bb70eca1-48a5-5370-90c6-ecf545de2948 
952 f f |p Can circulate  |a University of Colorado Boulder  |b Boulder Campus  |c Offsite  |d PASCAL Offsite  |e Y 3.N 21/5:6/4343  |h Superintendent of Documents classification  |i document  |m P204042110033  |n 1