Pressure distribution over a rectangular airfoil with a partial span split flap:
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Buch |
Sprache: | English |
Veröffentlicht: |
Washington
NACA
1936
|
Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Report
571 |
Beschreibung: | 12 S. Ill. graph. Darst. |
Internformat
MARC
LEADER | 00000nam a2200000 cb4500 | ||
---|---|---|---|
001 | BV013180791 | ||
003 | DE-604 | ||
005 | 00000000000000.0 | ||
007 | t | ||
008 | 000530s1936 ad|| t||| 00||| eng d | ||
035 | |a (DE-599)BVBBV013180791 | ||
040 | |a DE-604 |b ger |e rakwb | ||
041 | 0 | |a eng | |
088 | |a NACA TR 571 | ||
100 | 1 | |a Wenzinger, Carl J. |e Verfasser |4 aut | |
245 | 1 | 0 | |a Pressure distribution over a rectangular airfoil with a partial span split flap |c by Carl J. Wenzinger and Thomas A. Harris |
246 | 1 | 3 | |a NACA TR 571 |
264 | 1 | |a Washington |b NACA |c 1936 | |
300 | |a 12 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 571 | |
700 | 1 | |a Harris, Thomas A. |d 1910-1995 |e Verfasser |0 (DE-588)123804752 |4 aut | |
810 | 2 | |a National Advisory Committee for Aeronautics: Report |t United States |v 571 |w (DE-604)BV008910189 |9 571 | |
999 | |a oai:aleph.bib-bvb.de:BVB01-008980404 |
Datensatz im Suchindex
_version_ | 1804127881195945984 |
---|---|
any_adam_object | |
author | Wenzinger, Carl J. Harris, Thomas A. 1910-1995 |
author_GND | (DE-588)123804752 |
author_facet | Wenzinger, Carl J. Harris, Thomas A. 1910-1995 |
author_role | aut aut |
author_sort | Wenzinger, Carl J. |
author_variant | c j w cj cjw t a h ta tah |
building | Verbundindex |
bvnumber | BV013180791 |
ctrlnum | (DE-599)BVBBV013180791 |
format | Book |
fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01013nam a2200277 cb4500</leader><controlfield tag="001">BV013180791</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">00000000000000.0</controlfield><controlfield tag="007">t</controlfield><controlfield tag="008">000530s1936 ad|| t||| 00||| eng d</controlfield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV013180791</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 571</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Wenzinger, Carl J.</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Pressure distribution over a rectangular airfoil with a partial span split flap</subfield><subfield code="c">by Carl J. Wenzinger and Thomas A. Harris</subfield></datafield><datafield tag="246" ind1="1" ind2="3"><subfield code="a">NACA TR 571</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Washington</subfield><subfield code="b">NACA</subfield><subfield code="c">1936</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">12 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">571</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Harris, Thomas A.</subfield><subfield code="d">1910-1995</subfield><subfield code="e">Verfasser</subfield><subfield code="0">(DE-588)123804752</subfield><subfield code="4">aut</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">571</subfield><subfield code="w">(DE-604)BV008910189</subfield><subfield code="9">571</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-008980404</subfield></datafield></record></collection> |
id | DE-604.BV013180791 |
illustrated | Illustrated |
indexdate | 2024-07-09T18:40:23Z |
institution | BVB |
language | English |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-008980404 |
open_access_boolean | |
physical | 12 S. Ill. graph. Darst. |
publishDate | 1936 |
publishDateSearch | 1936 |
publishDateSort | 1936 |
publisher | NACA |
record_format | marc |
series2 | United States / National Advisory Committee for Aeronautics: Report |
spelling | Wenzinger, Carl J. Verfasser aut Pressure distribution over a rectangular airfoil with a partial span split flap by Carl J. Wenzinger and Thomas A. Harris NACA TR 571 Washington NACA 1936 12 S. Ill. graph. Darst. txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 571 Harris, Thomas A. 1910-1995 Verfasser (DE-588)123804752 aut National Advisory Committee for Aeronautics: Report United States 571 (DE-604)BV008910189 571 |
spellingShingle | Wenzinger, Carl J. Harris, Thomas A. 1910-1995 Pressure distribution over a rectangular airfoil with a partial span split flap |
title | Pressure distribution over a rectangular airfoil with a partial span split flap |
title_alt | NACA TR 571 |
title_auth | Pressure distribution over a rectangular airfoil with a partial span split flap |
title_exact_search | Pressure distribution over a rectangular airfoil with a partial span split flap |
title_full | Pressure distribution over a rectangular airfoil with a partial span split flap by Carl J. Wenzinger and Thomas A. Harris |
title_fullStr | Pressure distribution over a rectangular airfoil with a partial span split flap by Carl J. Wenzinger and Thomas A. Harris |
title_full_unstemmed | Pressure distribution over a rectangular airfoil with a partial span split flap by Carl J. Wenzinger and Thomas A. Harris |
title_short | Pressure distribution over a rectangular airfoil with a partial span split flap |
title_sort | pressure distribution over a rectangular airfoil with a partial span split flap |
volume_link | (DE-604)BV008910189 |
work_keys_str_mv | AT wenzingercarlj pressuredistributionoverarectangularairfoilwithapartialspansplitflap AT harristhomasa pressuredistributionoverarectangularairfoilwithapartialspansplitflap AT wenzingercarlj nacatr571 AT harristhomasa nacatr571 |