Investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles:
Gespeichert in:
1. Verfasser: | |
---|---|
Format: | Buch |
Sprache: | English |
Veröffentlicht: |
Washington
NACA
1955
|
Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Report
1238 |
Beschreibung: | 60 S. Ill., graph. Darst. |
Internformat
MARC
LEADER | 00000nam a2200000 cb4500 | ||
---|---|---|---|
001 | BV013244744 | ||
003 | DE-604 | ||
005 | 00000000000000.0 | ||
007 | t | ||
008 | 000711s1955 ad|| t||| 00||| eng d | ||
035 | |a (DE-599)BVBBV013244744 | ||
040 | |a DE-604 |b ger |e rakwb | ||
041 | 0 | |a eng | |
088 | |a NACA TR 1238 | ||
100 | 1 | |a Love, Eugene S. |e Verfasser |4 aut | |
245 | 1 | 0 | |a Investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles |c by Eugene S. Love |
246 | 1 | 3 | |a NACA TR 1238 |
264 | 1 | |a Washington |b NACA |c 1955 | |
300 | |a 60 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 1238 | |
810 | 2 | |a National Advisory Committee for Aeronautics: Report |t United States |v 1238 |w (DE-604)BV008910189 |9 1238 | |
999 | |a oai:aleph.bib-bvb.de:BVB01-009026949 |
Datensatz im Suchindex
_version_ | 1804128006369705984 |
---|---|
any_adam_object | |
author | Love, Eugene S. |
author_facet | Love, Eugene S. |
author_role | aut |
author_sort | Love, Eugene S. |
author_variant | e s l es esl |
building | Verbundindex |
bvnumber | BV013244744 |
ctrlnum | (DE-599)BVBBV013244744 |
format | Book |
fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>00951nam a2200265 cb4500</leader><controlfield tag="001">BV013244744</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">00000000000000.0</controlfield><controlfield tag="007">t</controlfield><controlfield tag="008">000711s1955 ad|| t||| 00||| eng d</controlfield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV013244744</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 1238</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Love, Eugene S.</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles</subfield><subfield code="c">by Eugene S. Love</subfield></datafield><datafield tag="246" ind1="1" ind2="3"><subfield code="a">NACA TR 1238</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Washington</subfield><subfield code="b">NACA</subfield><subfield code="c">1955</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">60 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">1238</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">1238</subfield><subfield code="w">(DE-604)BV008910189</subfield><subfield code="9">1238</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-009026949</subfield></datafield></record></collection> |
id | DE-604.BV013244744 |
illustrated | Illustrated |
indexdate | 2024-07-09T18:42:23Z |
institution | BVB |
language | English |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-009026949 |
open_access_boolean | |
physical | 60 S. Ill., graph. Darst. |
publishDate | 1955 |
publishDateSearch | 1955 |
publishDateSort | 1955 |
publisher | NACA |
record_format | marc |
series2 | United States / National Advisory Committee for Aeronautics: Report |
spelling | Love, Eugene S. Verfasser aut Investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles by Eugene S. Love NACA TR 1238 Washington NACA 1955 60 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 1238 National Advisory Committee for Aeronautics: Report United States 1238 (DE-604)BV008910189 1238 |
spellingShingle | Love, Eugene S. Investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles |
title | Investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles |
title_alt | NACA TR 1238 |
title_auth | Investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles |
title_exact_search | Investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles |
title_full | Investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles by Eugene S. Love |
title_fullStr | Investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles by Eugene S. Love |
title_full_unstemmed | Investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles by Eugene S. Love |
title_short | Investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles |
title_sort | investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles |
volume_link | (DE-604)BV008910189 |
work_keys_str_mv | AT loveeugenes investigationsatsupersonicspeedsof22triangularwingsrepresentingtwoairfoilsectionsforeachof11apexangles AT loveeugenes nacatr1238 |