A lift-cancellation technique in linearized supersonic-wing theory:
Saved in:
| Main Author: | |
|---|---|
| Format: | Book |
| Language: | English |
| Published: |
Washington, DC
US Gov. Print. Off.
1951
|
| Series: | United States / National Advisory Committee for Aeronautics: Report
1004 |
| Subjects: | |
| Physical Description: | 11 S. graph. Darst. 30 cm |
Staff View
MARC
| LEADER | 00000nam a2200000 cb4500 | ||
|---|---|---|---|
| 001 | BV035652988 | ||
| 003 | DE-604 | ||
| 005 | 20091020 | ||
| 007 | t | ||
| 008 | 090729s1951 d||| |||| 00||| eng d | ||
| 035 | |a (OCoLC)907902545 | ||
| 035 | |a (DE-599)BVBBV035652988 | ||
| 040 | |a DE-604 |b ger | ||
| 041 | 0 | |a eng | |
| 049 | |a DE-210 | ||
| 088 | |a NACA TR 1004 | ||
| 100 | 1 | |a Mirels, Harold |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a A lift-cancellation technique in linearized supersonic-wing theory |c by Harold Mirels |
| 246 | 1 | 3 | |a NACA TR 1004 |
| 264 | 1 | |a Washington, DC |b US Gov. Print. Off. |c 1951 | |
| 300 | |a 11 S. |b graph. Darst. |c 30 cm | ||
| 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 1004 | |
| 650 | 0 | 7 | |a Störung |0 (DE-588)4133232-5 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Auftrieb |0 (DE-588)4137274-8 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Überschallflugzeug |0 (DE-588)4186622-8 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Tragflügelaerodynamik |0 (DE-588)4185832-3 |2 gnd |9 rswk-swf |
| 689 | 0 | 0 | |a Überschallflugzeug |0 (DE-588)4186622-8 |D s |
| 689 | 0 | 1 | |a Tragflügelaerodynamik |0 (DE-588)4185832-3 |D s |
| 689 | 0 | |5 DE-604 | |
| 689 | 1 | 0 | |a Überschallflugzeug |0 (DE-588)4186622-8 |D s |
| 689 | 1 | 1 | |a Tragflügelaerodynamik |0 (DE-588)4185832-3 |D s |
| 689 | 1 | 2 | |a Auftrieb |0 (DE-588)4137274-8 |D s |
| 689 | 1 | 3 | |a Störung |0 (DE-588)4133232-5 |D s |
| 689 | 1 | |5 DE-604 | |
| 810 | 2 | |a National Advisory Committee for Aeronautics: Report |t United States |v 1004 |w (DE-604)BV008910189 |9 1004 | |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-017707542 | ||
Record in the Search Index
| _version_ | 1804139339468242944 |
|---|---|
| any_adam_object | |
| author | Mirels, Harold |
| author_facet | Mirels, Harold |
| author_role | aut |
| author_sort | Mirels, Harold |
| author_variant | h m hm |
| building | Verbundindex |
| bvnumber | BV035652988 |
| ctrlnum | (OCoLC)907902545 (DE-599)BVBBV035652988 |
| format | Book |
| fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01609nam a2200433 cb4500</leader><controlfield tag="001">BV035652988</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">20091020 </controlfield><controlfield tag="007">t</controlfield><controlfield tag="008">090729s1951 d||| |||| 00||| eng d</controlfield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)907902545</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV035652988</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-604</subfield><subfield code="b">ger</subfield></datafield><datafield tag="041" ind1="0" ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="049" ind1=" " ind2=" "><subfield code="a">DE-210</subfield></datafield><datafield tag="088" ind1=" " ind2=" "><subfield code="a">NACA TR 1004</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Mirels, Harold</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">A lift-cancellation technique in linearized supersonic-wing theory</subfield><subfield code="c">by Harold Mirels</subfield></datafield><datafield tag="246" ind1="1" ind2="3"><subfield code="a">NACA TR 1004</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Washington, DC</subfield><subfield code="b">US Gov. Print. Off.</subfield><subfield code="c">1951</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">11 S.</subfield><subfield code="b">graph. Darst.</subfield><subfield code="c">30 cm</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">1004</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Störung</subfield><subfield code="0">(DE-588)4133232-5</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Auftrieb</subfield><subfield code="0">(DE-588)4137274-8</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Überschallflugzeug</subfield><subfield code="0">(DE-588)4186622-8</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Tragflügelaerodynamik</subfield><subfield code="0">(DE-588)4185832-3</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="689" ind1="0" ind2="0"><subfield code="a">Überschallflugzeug</subfield><subfield code="0">(DE-588)4186622-8</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2="1"><subfield code="a">Tragflügelaerodynamik</subfield><subfield code="0">(DE-588)4185832-3</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="1" ind2="0"><subfield code="a">Überschallflugzeug</subfield><subfield code="0">(DE-588)4186622-8</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="1" ind2="1"><subfield code="a">Tragflügelaerodynamik</subfield><subfield code="0">(DE-588)4185832-3</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="1" ind2="2"><subfield code="a">Auftrieb</subfield><subfield code="0">(DE-588)4137274-8</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="1" ind2="3"><subfield code="a">Störung</subfield><subfield code="0">(DE-588)4133232-5</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="1" ind2=" "><subfield code="5">DE-604</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">1004</subfield><subfield code="w">(DE-604)BV008910189</subfield><subfield code="9">1004</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-017707542</subfield></datafield></record></collection> |
| id | DE-604.BV035652988 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T21:42:31Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-017707542 |
| oclc_num | 907902545 |
| open_access_boolean | |
| owner | DE-210 |
| owner_facet | DE-210 |
| physical | 11 S. graph. Darst. 30 cm |
| publishDate | 1951 |
| publishDateSearch | 1951 |
| publishDateSort | 1951 |
| publisher | US Gov. Print. Off. |
| record_format | marc |
| series2 | United States / National Advisory Committee for Aeronautics: Report |
| spelling | Mirels, Harold Verfasser aut A lift-cancellation technique in linearized supersonic-wing theory by Harold Mirels NACA TR 1004 Washington, DC US Gov. Print. Off. 1951 11 S. graph. Darst. 30 cm txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 1004 Störung (DE-588)4133232-5 gnd rswk-swf Auftrieb (DE-588)4137274-8 gnd rswk-swf Überschallflugzeug (DE-588)4186622-8 gnd rswk-swf Tragflügelaerodynamik (DE-588)4185832-3 gnd rswk-swf Überschallflugzeug (DE-588)4186622-8 s Tragflügelaerodynamik (DE-588)4185832-3 s DE-604 Auftrieb (DE-588)4137274-8 s Störung (DE-588)4133232-5 s National Advisory Committee for Aeronautics: Report United States 1004 (DE-604)BV008910189 1004 |
| spellingShingle | Mirels, Harold A lift-cancellation technique in linearized supersonic-wing theory Störung (DE-588)4133232-5 gnd Auftrieb (DE-588)4137274-8 gnd Überschallflugzeug (DE-588)4186622-8 gnd Tragflügelaerodynamik (DE-588)4185832-3 gnd |
| subject_GND | (DE-588)4133232-5 (DE-588)4137274-8 (DE-588)4186622-8 (DE-588)4185832-3 |
| title | A lift-cancellation technique in linearized supersonic-wing theory |
| title_alt | NACA TR 1004 |
| title_auth | A lift-cancellation technique in linearized supersonic-wing theory |
| title_exact_search | A lift-cancellation technique in linearized supersonic-wing theory |
| title_full | A lift-cancellation technique in linearized supersonic-wing theory by Harold Mirels |
| title_fullStr | A lift-cancellation technique in linearized supersonic-wing theory by Harold Mirels |
| title_full_unstemmed | A lift-cancellation technique in linearized supersonic-wing theory by Harold Mirels |
| title_short | A lift-cancellation technique in linearized supersonic-wing theory |
| title_sort | a lift cancellation technique in linearized supersonic wing theory |
| topic | Störung (DE-588)4133232-5 gnd Auftrieb (DE-588)4137274-8 gnd Überschallflugzeug (DE-588)4186622-8 gnd Tragflügelaerodynamik (DE-588)4185832-3 gnd |
| topic_facet | Störung Auftrieb Überschallflugzeug Tragflügelaerodynamik |
| volume_link | (DE-604)BV008910189 |
| work_keys_str_mv | AT mirelsharold aliftcancellationtechniqueinlinearizedsupersonicwingtheory AT mirelsharold nacatr1004 |