Aerothermodynamics of gas turbine and rocket propulsion:
Gespeichert in:
1. Verfasser: | |
---|---|
Format: | Buch |
Sprache: | English |
Veröffentlicht: |
New York, NY
American Inst. of Aeronautics and Astronautics, Inc.
1984
|
Schriftenreihe: | AIAA education series.
|
Schlagworte: | |
Beschreibung: | XII, 412 S. graph. Darst. |
ISBN: | 0915928876 |
Internformat
MARC
LEADER | 00000nam a2200000 c 4500 | ||
---|---|---|---|
001 | BV002191947 | ||
003 | DE-604 | ||
005 | 00000000000000.0 | ||
007 | t | ||
008 | 890928s1984 d||| |||| 00||| eng d | ||
020 | |a 0915928876 |9 0-915928-87-6 | ||
035 | |a (OCoLC)10799620 | ||
035 | |a (DE-599)BVBBV002191947 | ||
040 | |a DE-604 |b ger |e rakddb | ||
041 | 0 | |a eng | |
049 | |a DE-91 |a DE-91G |a DE-83 | ||
050 | 0 | |a TL574.A45 | |
082 | 0 | |a 629.1/2 |2 19 | |
084 | |a VER 720f |2 stub | ||
084 | |a MAS 585f |2 stub | ||
100 | 1 | |a Oates, Gordon C. |e Verfasser |4 aut | |
245 | 1 | 0 | |a Aerothermodynamics of gas turbine and rocket propulsion |
264 | 1 | |a New York, NY |b American Inst. of Aeronautics and Astronautics, Inc. |c 1984 | |
300 | |a XII, 412 S. |b graph. Darst. | ||
336 | |b txt |2 rdacontent | ||
337 | |b n |2 rdamedia | ||
338 | |b nc |2 rdacarrier | ||
490 | 0 | |a AIAA education series. | |
650 | 4 | |a Aerothermodynamics | |
650 | 4 | |a Aircraft gas-turbines | |
650 | 4 | |a Rocket engines | |
650 | 0 | 7 | |a Raketentriebwerk |0 (DE-588)4176905-3 |2 gnd |9 rswk-swf |
650 | 0 | 7 | |a Fluggasturbine |0 (DE-588)4278933-3 |2 gnd |9 rswk-swf |
650 | 0 | 7 | |a Aerothermodynamik |0 (DE-588)4133168-0 |2 gnd |9 rswk-swf |
650 | 0 | 7 | |a Aerodynamik |0 (DE-588)4000589-6 |2 gnd |9 rswk-swf |
650 | 0 | 7 | |a Gasturbine |0 (DE-588)4019416-4 |2 gnd |9 rswk-swf |
650 | 0 | 7 | |a Thermodynamik |0 (DE-588)4059827-5 |2 gnd |9 rswk-swf |
689 | 0 | 0 | |a Raketentriebwerk |0 (DE-588)4176905-3 |D s |
689 | 0 | 1 | |a Aerodynamik |0 (DE-588)4000589-6 |D s |
689 | 0 | |5 DE-604 | |
689 | 1 | 0 | |a Raketentriebwerk |0 (DE-588)4176905-3 |D s |
689 | 1 | 1 | |a Thermodynamik |0 (DE-588)4059827-5 |D s |
689 | 1 | |5 DE-604 | |
689 | 2 | 0 | |a Gasturbine |0 (DE-588)4019416-4 |D s |
689 | 2 | 1 | |a Aerodynamik |0 (DE-588)4000589-6 |D s |
689 | 2 | |5 DE-604 | |
689 | 3 | 0 | |a Gasturbine |0 (DE-588)4019416-4 |D s |
689 | 3 | 1 | |a Thermodynamik |0 (DE-588)4059827-5 |D s |
689 | 3 | |5 DE-604 | |
689 | 4 | 0 | |a Raketentriebwerk |0 (DE-588)4176905-3 |D s |
689 | 4 | 1 | |a Aerothermodynamik |0 (DE-588)4133168-0 |D s |
689 | 4 | 2 | |a Fluggasturbine |0 (DE-588)4278933-3 |D s |
689 | 4 | |8 1\p |5 DE-604 | |
940 | 1 | |q TUB-nveb | |
999 | |a oai:aleph.bib-bvb.de:BVB01-001439800 | ||
883 | 1 | |8 1\p |a cgwrk |d 20201028 |q DE-101 |u https://d-nb.info/provenance/plan#cgwrk |
Datensatz im Suchindex
_version_ | 1804116647289552896 |
---|---|
any_adam_object | |
author | Oates, Gordon C. |
author_facet | Oates, Gordon C. |
author_role | aut |
author_sort | Oates, Gordon C. |
author_variant | g c o gc gco |
building | Verbundindex |
bvnumber | BV002191947 |
callnumber-first | T - Technology |
callnumber-label | TL574 |
callnumber-raw | TL574.A45 |
callnumber-search | TL574.A45 |
callnumber-sort | TL 3574 A45 |
callnumber-subject | TL - Motor Vehicles and Aeronautics |
classification_tum | VER 720f MAS 585f |
ctrlnum | (OCoLC)10799620 (DE-599)BVBBV002191947 |
dewey-full | 629.1/2 |
dewey-hundreds | 600 - Technology (Applied sciences) |
dewey-ones | 629 - Other branches of engineering |
dewey-raw | 629.1/2 |
dewey-search | 629.1/2 |
dewey-sort | 3629.1 12 |
dewey-tens | 620 - Engineering and allied operations |
discipline | Verkehrstechnik Verkehr / Transport Maschinenbau |
format | Book |
fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>02221nam a2200637 c 4500</leader><controlfield tag="001">BV002191947</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">00000000000000.0</controlfield><controlfield tag="007">t</controlfield><controlfield tag="008">890928s1984 d||| |||| 00||| eng d</controlfield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">0915928876</subfield><subfield code="9">0-915928-87-6</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)10799620</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV002191947</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-604</subfield><subfield code="b">ger</subfield><subfield code="e">rakddb</subfield></datafield><datafield tag="041" ind1="0" ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="049" ind1=" " ind2=" "><subfield code="a">DE-91</subfield><subfield code="a">DE-91G</subfield><subfield code="a">DE-83</subfield></datafield><datafield tag="050" ind1=" " ind2="0"><subfield code="a">TL574.A45</subfield></datafield><datafield tag="082" ind1="0" ind2=" "><subfield code="a">629.1/2</subfield><subfield code="2">19</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">VER 720f</subfield><subfield code="2">stub</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">MAS 585f</subfield><subfield code="2">stub</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Oates, Gordon C.</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Aerothermodynamics of gas turbine and rocket propulsion</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">New York, NY</subfield><subfield code="b">American Inst. of Aeronautics and Astronautics, Inc.</subfield><subfield code="c">1984</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">XII, 412 S.</subfield><subfield code="b">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="0" ind2=" "><subfield code="a">AIAA education series.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Aerothermodynamics</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Aircraft gas-turbines</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Rocket engines</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Raketentriebwerk</subfield><subfield code="0">(DE-588)4176905-3</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Fluggasturbine</subfield><subfield code="0">(DE-588)4278933-3</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Aerothermodynamik</subfield><subfield code="0">(DE-588)4133168-0</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Aerodynamik</subfield><subfield code="0">(DE-588)4000589-6</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Gasturbine</subfield><subfield code="0">(DE-588)4019416-4</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Thermodynamik</subfield><subfield code="0">(DE-588)4059827-5</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="689" ind1="0" ind2="0"><subfield code="a">Raketentriebwerk</subfield><subfield code="0">(DE-588)4176905-3</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2="1"><subfield code="a">Aerodynamik</subfield><subfield code="0">(DE-588)4000589-6</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">Raketentriebwerk</subfield><subfield code="0">(DE-588)4176905-3</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="1" ind2="1"><subfield code="a">Thermodynamik</subfield><subfield code="0">(DE-588)4059827-5</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="1" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="2" ind2="0"><subfield code="a">Gasturbine</subfield><subfield code="0">(DE-588)4019416-4</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="2" ind2="1"><subfield code="a">Aerodynamik</subfield><subfield code="0">(DE-588)4000589-6</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="2" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="3" ind2="0"><subfield code="a">Gasturbine</subfield><subfield code="0">(DE-588)4019416-4</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="3" ind2="1"><subfield code="a">Thermodynamik</subfield><subfield code="0">(DE-588)4059827-5</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="3" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="4" ind2="0"><subfield code="a">Raketentriebwerk</subfield><subfield code="0">(DE-588)4176905-3</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="4" ind2="1"><subfield code="a">Aerothermodynamik</subfield><subfield code="0">(DE-588)4133168-0</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="4" ind2="2"><subfield code="a">Fluggasturbine</subfield><subfield code="0">(DE-588)4278933-3</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="4" ind2=" "><subfield code="8">1\p</subfield><subfield code="5">DE-604</subfield></datafield><datafield tag="940" ind1="1" ind2=" "><subfield code="q">TUB-nveb</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-001439800</subfield></datafield><datafield tag="883" ind1="1" ind2=" "><subfield code="8">1\p</subfield><subfield code="a">cgwrk</subfield><subfield code="d">20201028</subfield><subfield code="q">DE-101</subfield><subfield code="u">https://d-nb.info/provenance/plan#cgwrk</subfield></datafield></record></collection> |
id | DE-604.BV002191947 |
illustrated | Illustrated |
indexdate | 2024-07-09T15:41:50Z |
institution | BVB |
isbn | 0915928876 |
language | English |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-001439800 |
oclc_num | 10799620 |
open_access_boolean | |
owner | DE-91 DE-BY-TUM DE-91G DE-BY-TUM DE-83 |
owner_facet | DE-91 DE-BY-TUM DE-91G DE-BY-TUM DE-83 |
physical | XII, 412 S. graph. Darst. |
psigel | TUB-nveb |
publishDate | 1984 |
publishDateSearch | 1984 |
publishDateSort | 1984 |
publisher | American Inst. of Aeronautics and Astronautics, Inc. |
record_format | marc |
series2 | AIAA education series. |
spelling | Oates, Gordon C. Verfasser aut Aerothermodynamics of gas turbine and rocket propulsion New York, NY American Inst. of Aeronautics and Astronautics, Inc. 1984 XII, 412 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier AIAA education series. Aerothermodynamics Aircraft gas-turbines Rocket engines Raketentriebwerk (DE-588)4176905-3 gnd rswk-swf Fluggasturbine (DE-588)4278933-3 gnd rswk-swf Aerothermodynamik (DE-588)4133168-0 gnd rswk-swf Aerodynamik (DE-588)4000589-6 gnd rswk-swf Gasturbine (DE-588)4019416-4 gnd rswk-swf Thermodynamik (DE-588)4059827-5 gnd rswk-swf Raketentriebwerk (DE-588)4176905-3 s Aerodynamik (DE-588)4000589-6 s DE-604 Thermodynamik (DE-588)4059827-5 s Gasturbine (DE-588)4019416-4 s Aerothermodynamik (DE-588)4133168-0 s Fluggasturbine (DE-588)4278933-3 s 1\p DE-604 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk |
spellingShingle | Oates, Gordon C. Aerothermodynamics of gas turbine and rocket propulsion Aerothermodynamics Aircraft gas-turbines Rocket engines Raketentriebwerk (DE-588)4176905-3 gnd Fluggasturbine (DE-588)4278933-3 gnd Aerothermodynamik (DE-588)4133168-0 gnd Aerodynamik (DE-588)4000589-6 gnd Gasturbine (DE-588)4019416-4 gnd Thermodynamik (DE-588)4059827-5 gnd |
subject_GND | (DE-588)4176905-3 (DE-588)4278933-3 (DE-588)4133168-0 (DE-588)4000589-6 (DE-588)4019416-4 (DE-588)4059827-5 |
title | Aerothermodynamics of gas turbine and rocket propulsion |
title_auth | Aerothermodynamics of gas turbine and rocket propulsion |
title_exact_search | Aerothermodynamics of gas turbine and rocket propulsion |
title_full | Aerothermodynamics of gas turbine and rocket propulsion |
title_fullStr | Aerothermodynamics of gas turbine and rocket propulsion |
title_full_unstemmed | Aerothermodynamics of gas turbine and rocket propulsion |
title_short | Aerothermodynamics of gas turbine and rocket propulsion |
title_sort | aerothermodynamics of gas turbine and rocket propulsion |
topic | Aerothermodynamics Aircraft gas-turbines Rocket engines Raketentriebwerk (DE-588)4176905-3 gnd Fluggasturbine (DE-588)4278933-3 gnd Aerothermodynamik (DE-588)4133168-0 gnd Aerodynamik (DE-588)4000589-6 gnd Gasturbine (DE-588)4019416-4 gnd Thermodynamik (DE-588)4059827-5 gnd |
topic_facet | Aerothermodynamics Aircraft gas-turbines Rocket engines Raketentriebwerk Fluggasturbine Aerothermodynamik Aerodynamik Gasturbine Thermodynamik |
work_keys_str_mv | AT oatesgordonc aerothermodynamicsofgasturbineandrocketpropulsion |