A method for determing the camber and twist of a surface to support a given distribution of lift, with applications to the load over a sweptback wing:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Washington
NACA
1945
|
| Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Report
826 |
| Beschreibung: | 10 S. Ill., graph. Darst. |
Internformat
MARC
| LEADER | 00000nam a2200000 cb4500 | ||
|---|---|---|---|
| 001 | BV013239691 | ||
| 003 | DE-604 | ||
| 005 | 00000000000000.0 | ||
| 007 | t | ||
| 008 | 000707s1945 ad|| t||| 00||| eng d | ||
| 035 | |a (DE-599)BVBBV013239691 | ||
| 040 | |a DE-604 |b ger |e rakwb | ||
| 041 | 0 | |a eng | |
| 088 | |a NACA TR 826 | ||
| 100 | 1 | |a Cohen, Doris |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a A method for determing the camber and twist of a surface to support a given distribution of lift, with applications to the load over a sweptback wing |c by Doris Cohen |
| 246 | 1 | 3 | |a NACA TR 826 |
| 264 | 1 | |a Washington |b NACA |c 1945 | |
| 300 | |a 10 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 826 | |
| 810 | 2 | |a National Advisory Committee for Aeronautics: Report |t United States |v 826 |w (DE-604)BV008910189 |9 826 | |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-009022383 | ||
Datensatz im Suchindex
| _version_ | 1804127999569690624 |
|---|---|
| any_adam_object | |
| author | Cohen, Doris |
| author_facet | Cohen, Doris |
| author_role | aut |
| author_sort | Cohen, Doris |
| author_variant | d c dc |
| building | Verbundindex |
| bvnumber | BV013239691 |
| ctrlnum | (DE-599)BVBBV013239691 |
| format | Book |
| fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>00975nam a2200265 cb4500</leader><controlfield tag="001">BV013239691</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">00000000000000.0</controlfield><controlfield tag="007">t</controlfield><controlfield tag="008">000707s1945 ad|| t||| 00||| eng d</controlfield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV013239691</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 826</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Cohen, Doris</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">A method for determing the camber and twist of a surface to support a given distribution of lift, with applications to the load over a sweptback wing</subfield><subfield code="c">by Doris Cohen</subfield></datafield><datafield tag="246" ind1="1" ind2="3"><subfield code="a">NACA TR 826</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Washington</subfield><subfield code="b">NACA</subfield><subfield code="c">1945</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">10 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">826</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">826</subfield><subfield code="w">(DE-604)BV008910189</subfield><subfield code="9">826</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-009022383</subfield></datafield></record></collection> |
| id | DE-604.BV013239691 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T18:42:16Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-009022383 |
| open_access_boolean | |
| physical | 10 S. Ill., graph. Darst. |
| publishDate | 1945 |
| publishDateSearch | 1945 |
| publishDateSort | 1945 |
| publisher | NACA |
| record_format | marc |
| series2 | United States / National Advisory Committee for Aeronautics: Report |
| spelling | Cohen, Doris Verfasser aut A method for determing the camber and twist of a surface to support a given distribution of lift, with applications to the load over a sweptback wing by Doris Cohen NACA TR 826 Washington NACA 1945 10 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 826 National Advisory Committee for Aeronautics: Report United States 826 (DE-604)BV008910189 826 |
| spellingShingle | Cohen, Doris A method for determing the camber and twist of a surface to support a given distribution of lift, with applications to the load over a sweptback wing |
| title | A method for determing the camber and twist of a surface to support a given distribution of lift, with applications to the load over a sweptback wing |
| title_alt | NACA TR 826 |
| title_auth | A method for determing the camber and twist of a surface to support a given distribution of lift, with applications to the load over a sweptback wing |
| title_exact_search | A method for determing the camber and twist of a surface to support a given distribution of lift, with applications to the load over a sweptback wing |
| title_full | A method for determing the camber and twist of a surface to support a given distribution of lift, with applications to the load over a sweptback wing by Doris Cohen |
| title_fullStr | A method for determing the camber and twist of a surface to support a given distribution of lift, with applications to the load over a sweptback wing by Doris Cohen |
| title_full_unstemmed | A method for determing the camber and twist of a surface to support a given distribution of lift, with applications to the load over a sweptback wing by Doris Cohen |
| title_short | A method for determing the camber and twist of a surface to support a given distribution of lift, with applications to the load over a sweptback wing |
| title_sort | a method for determing the camber and twist of a surface to support a given distribution of lift with applications to the load over a sweptback wing |
| volume_link | (DE-604)BV008910189 |
| work_keys_str_mv | AT cohendoris amethodfordetermingthecamberandtwistofasurfacetosupportagivendistributionofliftwithapplicationstotheloadoverasweptbackwing AT cohendoris nacatr826 |