A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Washington
NACA
1958
|
| Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Report
1372 |
| Beschreibung: | 21 S. Ill., graph. Darst. |
Internformat
MARC
| LEADER | 00000nam a2200000 cb4500 | ||
|---|---|---|---|
| 001 | BV013396606 | ||
| 003 | DE-604 | ||
| 005 | 00000000000000.0 | ||
| 007 | t | ||
| 008 | 001020s1958 ad|| t||| 00||| eng d | ||
| 035 | |a (DE-599)BVBBV013396606 | ||
| 040 | |a DE-604 |b ger |e rakwb | ||
| 041 | 0 | |a eng | |
| 088 | |a NACA TR 1372 | ||
| 100 | 1 | |a Hill, P. R. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient |c by P. R. Hill |
| 246 | 1 | 3 | |a NACA TR 1372 |
| 264 | 1 | |a Washington |b NACA |c 1958 | |
| 300 | |a 21 S. |b Ill., graph. Darst. | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 490 | 1 | |a United States / National Advisory Committee for Aeronautics: Report |v 1372 | |
| 810 | 2 | |a National Advisory Committee for Aeronautics: Report |t United States |v 1372 |w (DE-604)BV008910189 |9 1372 | |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-009139684 | ||
Datensatz im Suchindex
| _version_ | 1804128179823050752 |
|---|---|
| any_adam_object | |
| author | Hill, P. R. |
| author_facet | Hill, P. R. |
| author_role | aut |
| author_sort | Hill, P. R. |
| author_variant | p r h pr prh |
| building | Verbundindex |
| bvnumber | BV013396606 |
| ctrlnum | (DE-599)BVBBV013396606 |
| format | Book |
| fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>00976nam a2200265 cb4500</leader><controlfield tag="001">BV013396606</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">00000000000000.0</controlfield><controlfield tag="007">t</controlfield><controlfield tag="008">001020s1958 ad|| t||| 00||| eng d</controlfield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV013396606</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-604</subfield><subfield code="b">ger</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1="0" ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="088" ind1=" " ind2=" "><subfield code="a">NACA TR 1372</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Hill, P. R.</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient</subfield><subfield code="c">by P. R. Hill</subfield></datafield><datafield tag="246" ind1="1" ind2="3"><subfield code="a">NACA TR 1372</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Washington</subfield><subfield code="b">NACA</subfield><subfield code="c">1958</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">21 S.</subfield><subfield code="b">Ill., graph. Darst.</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="490" ind1="1" ind2=" "><subfield code="a">United States / National Advisory Committee for Aeronautics: Report</subfield><subfield code="v">1372</subfield></datafield><datafield tag="810" ind1="2" ind2=" "><subfield code="a">National Advisory Committee for Aeronautics: Report</subfield><subfield code="t">United States</subfield><subfield code="v">1372</subfield><subfield code="w">(DE-604)BV008910189</subfield><subfield code="9">1372</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-009139684</subfield></datafield></record></collection> |
| id | DE-604.BV013396606 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T18:45:08Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-009139684 |
| open_access_boolean | |
| physical | 21 S. Ill., graph. Darst. |
| publishDate | 1958 |
| publishDateSearch | 1958 |
| publishDateSort | 1958 |
| publisher | NACA |
| record_format | marc |
| series2 | United States / National Advisory Committee for Aeronautics: Report |
| spelling | Hill, P. R. Verfasser aut A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient by P. R. Hill NACA TR 1372 Washington NACA 1958 21 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 1372 National Advisory Committee for Aeronautics: Report United States 1372 (DE-604)BV008910189 1372 |
| spellingShingle | Hill, P. R. A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient |
| title | A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient |
| title_alt | NACA TR 1372 |
| title_auth | A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient |
| title_exact_search | A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient |
| title_full | A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient by P. R. Hill |
| title_fullStr | A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient by P. R. Hill |
| title_full_unstemmed | A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient by P. R. Hill |
| title_short | A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient |
| title_sort | a method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient |
| volume_link | (DE-604)BV008910189 |
| work_keys_str_mv | AT hillpr amethodofcomputingthetransienttemperatureofthickwallsfromarbitraryvariationofadiabaticwalltemperatureandheattransfercoefficient AT hillpr nacatr1372 |