Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta-wing model:
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Washington
NACA
1955
|
| Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Report
1224 |
| Beschreibung: | 31 S. Ill., graph. Darst. |
Internformat
MARC
| LEADER | 00000nam a2200000 cb4500 | ||
|---|---|---|---|
| 001 | BV013243288 | ||
| 003 | DE-604 | ||
| 005 | 00000000000000.0 | ||
| 007 | t | ||
| 008 | 000711s1955 ad|| t||| 00||| eng d | ||
| 035 | |a (DE-599)BVBBV013243288 | ||
| 040 | |a DE-604 |b ger |e rakwb | ||
| 041 | 0 | |a eng | |
| 088 | |a NACA TR 1224 | ||
| 100 | 1 | |a Goodman, Alex |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta-wing model |c by Alex Goodman and David F. Thomas |
| 246 | 1 | 3 | |a NACA TR 1224 |
| 264 | 1 | |a Washington |b NACA |c 1955 | |
| 300 | |a 31 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 1224 | |
| 700 | 1 | |a Thomas, David F. |e Verfasser |4 aut | |
| 810 | 2 | |a National Advisory Committee for Aeronautics: Report |t United States |v 1224 |w (DE-604)BV008910189 |9 1224 | |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-009025617 | ||
Datensatz im Suchindex
| _version_ | 1804128004455006208 |
|---|---|
| any_adam_object | |
| author | Goodman, Alex Thomas, David F. |
| author_facet | Goodman, Alex Thomas, David F. |
| author_role | aut aut |
| author_sort | Goodman, Alex |
| author_variant | a g ag d f t df dft |
| building | Verbundindex |
| bvnumber | BV013243288 |
| ctrlnum | (DE-599)BVBBV013243288 |
| format | Book |
| fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01024nam a2200277 cb4500</leader><controlfield tag="001">BV013243288</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)BVBBV013243288</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 1224</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Goodman, Alex</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta-wing model</subfield><subfield code="c">by Alex Goodman and David F. Thomas</subfield></datafield><datafield tag="246" ind1="1" ind2="3"><subfield code="a">NACA TR 1224</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">31 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">1224</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Thomas, David F.</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">1224</subfield><subfield code="w">(DE-604)BV008910189</subfield><subfield code="9">1224</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-009025617</subfield></datafield></record></collection> |
| id | DE-604.BV013243288 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T18:42:21Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-009025617 |
| open_access_boolean | |
| physical | 31 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 | Goodman, Alex Verfasser aut Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta-wing model by Alex Goodman and David F. Thomas NACA TR 1224 Washington NACA 1955 31 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 1224 Thomas, David F. Verfasser aut National Advisory Committee for Aeronautics: Report United States 1224 (DE-604)BV008910189 1224 |
| spellingShingle | Goodman, Alex Thomas, David F. Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta-wing model |
| title | Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta-wing model |
| title_alt | NACA TR 1224 |
| title_auth | Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta-wing model |
| title_exact_search | Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta-wing model |
| title_full | Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta-wing model by Alex Goodman and David F. Thomas |
| title_fullStr | Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta-wing model by Alex Goodman and David F. Thomas |
| title_full_unstemmed | Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta-wing model by Alex Goodman and David F. Thomas |
| title_short | Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta-wing model |
| title_sort | effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta wing model |
| volume_link | (DE-604)BV008910189 |
| work_keys_str_mv | AT goodmanalex effectsofwingpositionandfuselagesizeonthelowspeedstaticandrollingstabilitycharacteristicsofadeltawingmodel AT thomasdavidf effectsofwingpositionandfuselagesizeonthelowspeedstaticandrollingstabilitycharacteristicsofadeltawingmodel AT goodmanalex nacatr1224 AT thomasdavidf nacatr1224 |