Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection:
Gespeichert in:
Hauptverfasser: | , |
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Format: | Buch |
Sprache: | English |
Veröffentlicht: |
Washington, D.C.
National Advisory Committee for Aeronautics
1951
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Schriftenreihe: | Report / National Advisory Committee for Aeronautics
1006 |
Schlagworte: | |
Beschreibung: | ii, 20 Seiten Diagramme, Illustration 28 cm |
Internformat
MARC
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007 | t | ||
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035 | |a (OCoLC)774063691 | ||
035 | |a (DE-599)BVBBV044330219 | ||
040 | |a DE-604 |b ger |e rda | ||
041 | 0 | |a eng | |
049 | |a DE-706 | ||
100 | 1 | |a Wilcox, E. Clinton |e Verfasser |4 aut | |
245 | 1 | 0 | |a Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection |c by E. Clinton Wilcox and Arthur M. Trout (Lewis Flight Propulsion Laboratory, Cleveland, Ohio) |
264 | 1 | |a Washington, D.C. |b National Advisory Committee for Aeronautics |c 1951 | |
300 | |a ii, 20 Seiten |b Diagramme, Illustration |c 28 cm | ||
336 | |b txt |2 rdacontent | ||
337 | |b n |2 rdamedia | ||
338 | |b nc |2 rdacarrier | ||
490 | 1 | |a Report / National Advisory Committee for Aeronautics |v 1006 | |
650 | 0 | 7 | |a Wassereinspritzung |0 (DE-588)1241832277 |2 gnd |9 rswk-swf |
650 | 0 | 7 | |a Turboluftstrahltriebwerk |0 (DE-588)4133979-4 |2 gnd |9 rswk-swf |
650 | 0 | 7 | |a Flugmotor |0 (DE-588)4121282-4 |2 gnd |9 rswk-swf |
653 | 0 | |a Aeronautics / Research | |
653 | 0 | |a Airplanes / Turbojet engines | |
653 | 0 | |a Airplanes / Motors / Thrust | |
689 | 0 | 0 | |a Flugmotor |0 (DE-588)4121282-4 |D s |
689 | 0 | 1 | |a Turboluftstrahltriebwerk |0 (DE-588)4133979-4 |D s |
689 | 0 | 2 | |a Wassereinspritzung |0 (DE-588)1241832277 |D s |
689 | 0 | |5 DE-604 | |
700 | 1 | |a Trout, Arthur M. |e Verfasser |4 aut | |
810 | 2 | |a National Advisory Committee for Aeronautics |t Report |v 1006 |w (DE-604)BV008910189 |9 1006 | |
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Datensatz im Suchindex
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any_adam_object | |
author | Wilcox, E. Clinton Trout, Arthur M. |
author_facet | Wilcox, E. Clinton Trout, Arthur M. |
author_role | aut aut |
author_sort | Wilcox, E. Clinton |
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id | DE-604.BV044330219 |
illustrated | Illustrated |
indexdate | 2024-07-10T07:49:56Z |
institution | BVB |
language | English |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-029733499 |
oclc_num | 774063691 |
open_access_boolean | |
owner | DE-706 |
owner_facet | DE-706 |
physical | ii, 20 Seiten Diagramme, Illustration 28 cm |
publishDate | 1951 |
publishDateSearch | 1951 |
publishDateSort | 1951 |
publisher | National Advisory Committee for Aeronautics |
record_format | marc |
series2 | Report / National Advisory Committee for Aeronautics |
spelling | Wilcox, E. Clinton Verfasser aut Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection by E. Clinton Wilcox and Arthur M. Trout (Lewis Flight Propulsion Laboratory, Cleveland, Ohio) Washington, D.C. National Advisory Committee for Aeronautics 1951 ii, 20 Seiten Diagramme, Illustration 28 cm txt rdacontent n rdamedia nc rdacarrier Report / National Advisory Committee for Aeronautics 1006 Wassereinspritzung (DE-588)1241832277 gnd rswk-swf Turboluftstrahltriebwerk (DE-588)4133979-4 gnd rswk-swf Flugmotor (DE-588)4121282-4 gnd rswk-swf Aeronautics / Research Airplanes / Turbojet engines Airplanes / Motors / Thrust Flugmotor (DE-588)4121282-4 s Turboluftstrahltriebwerk (DE-588)4133979-4 s Wassereinspritzung (DE-588)1241832277 s DE-604 Trout, Arthur M. Verfasser aut National Advisory Committee for Aeronautics Report 1006 (DE-604)BV008910189 1006 |
spellingShingle | Wilcox, E. Clinton Trout, Arthur M. Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection Wassereinspritzung (DE-588)1241832277 gnd Turboluftstrahltriebwerk (DE-588)4133979-4 gnd Flugmotor (DE-588)4121282-4 gnd |
subject_GND | (DE-588)1241832277 (DE-588)4133979-4 (DE-588)4121282-4 |
title | Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection |
title_auth | Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection |
title_exact_search | Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection |
title_full | Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection by E. Clinton Wilcox and Arthur M. Trout (Lewis Flight Propulsion Laboratory, Cleveland, Ohio) |
title_fullStr | Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection by E. Clinton Wilcox and Arthur M. Trout (Lewis Flight Propulsion Laboratory, Cleveland, Ohio) |
title_full_unstemmed | Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection by E. Clinton Wilcox and Arthur M. Trout (Lewis Flight Propulsion Laboratory, Cleveland, Ohio) |
title_short | Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection |
title_sort | analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection |
topic | Wassereinspritzung (DE-588)1241832277 gnd Turboluftstrahltriebwerk (DE-588)4133979-4 gnd Flugmotor (DE-588)4121282-4 gnd |
topic_facet | Wassereinspritzung Turboluftstrahltriebwerk Flugmotor |
volume_link | (DE-604)BV008910189 |
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