A second-order schock expansion method applicable to bodies of revolution near zero lift:
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Buch |
Sprache: | English |
Veröffentlicht: |
Washington
NACA
1957
|
Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Report
1328 |
Beschreibung: | 20 S. Ill., graph. Darst. |
Internformat
MARC
LEADER | 00000nam a2200000 cb4500 | ||
---|---|---|---|
001 | BV013255498 | ||
003 | DE-604 | ||
005 | 00000000000000.0 | ||
007 | t | ||
008 | 000718s1957 ad|| t||| 00||| eng d | ||
035 | |a (DE-599)BVBBV013255498 | ||
040 | |a DE-604 |b ger |e rakwb | ||
041 | 0 | |a eng | |
088 | |a NACA TR 1328 | ||
100 | 1 | |a Syvertson, Clarence A. |e Verfasser |4 aut | |
245 | 1 | 0 | |a A second-order schock expansion method applicable to bodies of revolution near zero lift |c by Clarence A. Syvertson and David H. Dennis |
246 | 1 | 3 | |a NACA TR 1328 |
264 | 1 | |a Washington |b NACA |c 1957 | |
300 | |a 20 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 1328 | |
700 | 1 | |a Dennis, David H. |e Verfasser |4 aut | |
810 | 2 | |a National Advisory Committee for Aeronautics: Report |t United States |v 1328 |w (DE-604)BV008910189 |9 1328 | |
999 | |a oai:aleph.bib-bvb.de:BVB01-009035472 |
Datensatz im Suchindex
_version_ | 1804128019195887616 |
---|---|
any_adam_object | |
author | Syvertson, Clarence A. Dennis, David H. |
author_facet | Syvertson, Clarence A. Dennis, David H. |
author_role | aut aut |
author_sort | Syvertson, Clarence A. |
author_variant | c a s ca cas d h d dh dhd |
building | Verbundindex |
bvnumber | BV013255498 |
ctrlnum | (DE-599)BVBBV013255498 |
format | Book |
fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01008nam a2200277 cb4500</leader><controlfield tag="001">BV013255498</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">00000000000000.0</controlfield><controlfield tag="007">t</controlfield><controlfield tag="008">000718s1957 ad|| t||| 00||| eng d</controlfield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV013255498</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 1328</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Syvertson, Clarence A.</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">A second-order schock expansion method applicable to bodies of revolution near zero lift</subfield><subfield code="c">by Clarence A. Syvertson and David H. Dennis</subfield></datafield><datafield tag="246" ind1="1" ind2="3"><subfield code="a">NACA TR 1328</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Washington</subfield><subfield code="b">NACA</subfield><subfield code="c">1957</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">20 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">1328</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Dennis, David H.</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">1328</subfield><subfield code="w">(DE-604)BV008910189</subfield><subfield code="9">1328</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-009035472</subfield></datafield></record></collection> |
id | DE-604.BV013255498 |
illustrated | Illustrated |
indexdate | 2024-07-09T18:42:35Z |
institution | BVB |
language | English |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-009035472 |
open_access_boolean | |
physical | 20 S. Ill., graph. Darst. |
publishDate | 1957 |
publishDateSearch | 1957 |
publishDateSort | 1957 |
publisher | NACA |
record_format | marc |
series2 | United States / National Advisory Committee for Aeronautics: Report |
spelling | Syvertson, Clarence A. Verfasser aut A second-order schock expansion method applicable to bodies of revolution near zero lift by Clarence A. Syvertson and David H. Dennis NACA TR 1328 Washington NACA 1957 20 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 1328 Dennis, David H. Verfasser aut National Advisory Committee for Aeronautics: Report United States 1328 (DE-604)BV008910189 1328 |
spellingShingle | Syvertson, Clarence A. Dennis, David H. A second-order schock expansion method applicable to bodies of revolution near zero lift |
title | A second-order schock expansion method applicable to bodies of revolution near zero lift |
title_alt | NACA TR 1328 |
title_auth | A second-order schock expansion method applicable to bodies of revolution near zero lift |
title_exact_search | A second-order schock expansion method applicable to bodies of revolution near zero lift |
title_full | A second-order schock expansion method applicable to bodies of revolution near zero lift by Clarence A. Syvertson and David H. Dennis |
title_fullStr | A second-order schock expansion method applicable to bodies of revolution near zero lift by Clarence A. Syvertson and David H. Dennis |
title_full_unstemmed | A second-order schock expansion method applicable to bodies of revolution near zero lift by Clarence A. Syvertson and David H. Dennis |
title_short | A second-order schock expansion method applicable to bodies of revolution near zero lift |
title_sort | a second order schock expansion method applicable to bodies of revolution near zero lift |
volume_link | (DE-604)BV008910189 |
work_keys_str_mv | AT syvertsonclarencea asecondorderschockexpansionmethodapplicabletobodiesofrevolutionnearzerolift AT dennisdavidh asecondorderschockexpansionmethodapplicabletobodiesofrevolutionnearzerolift AT syvertsonclarencea nacatr1328 AT dennisdavidh nacatr1328 |