Line-vortex theory for calculation of supersonic downwash:
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Washington, DC
US Gov. Print. Off.
1950
|
| Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Report
983 |
| Schlagworte: | |
| Beschreibung: | 13 S. graph. Darst. 30 cm |
Internformat
MARC
| LEADER | 00000nam a2200000 cb4500 | ||
|---|---|---|---|
| 001 | BV035653126 | ||
| 003 | DE-604 | ||
| 005 | 20091020 | ||
| 007 | t | ||
| 008 | 090729s1950 d||| |||| 00||| eng d | ||
| 035 | |a (OCoLC)907902607 | ||
| 035 | |a (DE-599)BVBBV035653126 | ||
| 040 | |a DE-604 |b ger | ||
| 041 | 0 | |a eng | |
| 049 | |a DE-210 | ||
| 088 | |a NACA TR 983 | ||
| 100 | 1 | |a Mirels, Harold |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Line-vortex theory for calculation of supersonic downwash |c by Harold Mirels and Rudolph C. Haeferli |
| 246 | 1 | 3 | |a NACA TR 983 |
| 264 | 1 | |a Washington, DC |b US Gov. Print. Off. |c 1950 | |
| 300 | |a 13 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 983 | |
| 650 | 0 | 7 | |a Tragflügelaerodynamik |0 (DE-588)4185832-3 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Überschallflugzeug |0 (DE-588)4186622-8 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Wirbel |g Physik |0 (DE-588)4128386-7 |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 | 2 | |a Wirbel |g Physik |0 (DE-588)4128386-7 |D s |
| 689 | 0 | |5 DE-604 | |
| 700 | 1 | |a Haefeli, Rudolph C. |e Verfasser |4 aut | |
| 810 | 2 | |a National Advisory Committee for Aeronautics: Report |t United States |v 983 |w (DE-604)BV008910189 |9 983 | |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-017707678 | ||
Datensatz im Suchindex
| _version_ | 1804139339688443904 |
|---|---|
| any_adam_object | |
| author | Mirels, Harold Haefeli, Rudolph C. |
| author_facet | Mirels, Harold Haefeli, Rudolph C. |
| author_role | aut aut |
| author_sort | Mirels, Harold |
| author_variant | h m hm r c h rc rch |
| building | Verbundindex |
| bvnumber | BV035653126 |
| ctrlnum | (OCoLC)907902607 (DE-599)BVBBV035653126 |
| format | Book |
| fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01431nam a2200385 cb4500</leader><controlfield tag="001">BV035653126</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">20091020 </controlfield><controlfield tag="007">t</controlfield><controlfield tag="008">090729s1950 d||| |||| 00||| eng d</controlfield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)907902607</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV035653126</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 983</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">Line-vortex theory for calculation of supersonic downwash</subfield><subfield code="c">by Harold Mirels and Rudolph C. Haeferli</subfield></datafield><datafield tag="246" ind1="1" ind2="3"><subfield code="a">NACA TR 983</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">1950</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">13 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">983</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="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">Wirbel</subfield><subfield code="g">Physik</subfield><subfield code="0">(DE-588)4128386-7</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="2"><subfield code="a">Wirbel</subfield><subfield code="g">Physik</subfield><subfield code="0">(DE-588)4128386-7</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Haefeli, Rudolph C.</subfield><subfield code="e">Verfasser</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">983</subfield><subfield code="w">(DE-604)BV008910189</subfield><subfield code="9">983</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-017707678</subfield></datafield></record></collection> |
| id | DE-604.BV035653126 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T21:42:31Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-017707678 |
| oclc_num | 907902607 |
| open_access_boolean | |
| owner | DE-210 |
| owner_facet | DE-210 |
| physical | 13 S. graph. Darst. 30 cm |
| publishDate | 1950 |
| publishDateSearch | 1950 |
| publishDateSort | 1950 |
| publisher | US Gov. Print. Off. |
| record_format | marc |
| series2 | United States / National Advisory Committee for Aeronautics: Report |
| spelling | Mirels, Harold Verfasser aut Line-vortex theory for calculation of supersonic downwash by Harold Mirels and Rudolph C. Haeferli NACA TR 983 Washington, DC US Gov. Print. Off. 1950 13 S. graph. Darst. 30 cm txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 983 Tragflügelaerodynamik (DE-588)4185832-3 gnd rswk-swf Überschallflugzeug (DE-588)4186622-8 gnd rswk-swf Wirbel Physik (DE-588)4128386-7 gnd rswk-swf Überschallflugzeug (DE-588)4186622-8 s Tragflügelaerodynamik (DE-588)4185832-3 s Wirbel Physik (DE-588)4128386-7 s DE-604 Haefeli, Rudolph C. Verfasser aut National Advisory Committee for Aeronautics: Report United States 983 (DE-604)BV008910189 983 |
| spellingShingle | Mirels, Harold Haefeli, Rudolph C. Line-vortex theory for calculation of supersonic downwash Tragflügelaerodynamik (DE-588)4185832-3 gnd Überschallflugzeug (DE-588)4186622-8 gnd Wirbel Physik (DE-588)4128386-7 gnd |
| subject_GND | (DE-588)4185832-3 (DE-588)4186622-8 (DE-588)4128386-7 |
| title | Line-vortex theory for calculation of supersonic downwash |
| title_alt | NACA TR 983 |
| title_auth | Line-vortex theory for calculation of supersonic downwash |
| title_exact_search | Line-vortex theory for calculation of supersonic downwash |
| title_full | Line-vortex theory for calculation of supersonic downwash by Harold Mirels and Rudolph C. Haeferli |
| title_fullStr | Line-vortex theory for calculation of supersonic downwash by Harold Mirels and Rudolph C. Haeferli |
| title_full_unstemmed | Line-vortex theory for calculation of supersonic downwash by Harold Mirels and Rudolph C. Haeferli |
| title_short | Line-vortex theory for calculation of supersonic downwash |
| title_sort | line vortex theory for calculation of supersonic downwash |
| topic | Tragflügelaerodynamik (DE-588)4185832-3 gnd Überschallflugzeug (DE-588)4186622-8 gnd Wirbel Physik (DE-588)4128386-7 gnd |
| topic_facet | Tragflügelaerodynamik Überschallflugzeug Wirbel Physik |
| volume_link | (DE-604)BV008910189 |
| work_keys_str_mv | AT mirelsharold linevortextheoryforcalculationofsupersonicdownwash AT haefelirudolphc linevortextheoryforcalculationofsupersonicdownwash AT mirelsharold nacatr983 AT haefelirudolphc nacatr983 |