The Resource Redesign of the low speed three stage axial flow compressor test facility, by M.H. Vavra, P.F. Pucci [and] W. Schlachter
Redesign of the low speed three stage axial flow compressor test facility, by M.H. Vavra, P.F. Pucci [and] W. Schlachter
Resource Information
The item Redesign of the low speed three stage axial flow compressor test facility, by M.H. Vavra, P.F. Pucci [and] W. Schlachter represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Internet Archive - Open Library.This item is available to borrow from all library branches.
Resource Information
The item Redesign of the low speed three stage axial flow compressor test facility, by M.H. Vavra, P.F. Pucci [and] W. Schlachter represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Internet Archive - Open Library.
This item is available to borrow from all library branches.
- Summary
- A flow configuration of an existing low-speed, axial flow compressor test facility at the Turbopropulsion Laboratory, Naval Postgarduate School, Monterey, California, was redesigned in order to improve compressor inlet velocity distribution, improve mass flow measurement, and increase the power input. The design of the new configuration, consisting of an inlet nozzle, ducting, throttling device upstream of the compressor, and a diffusor downstream of it, is reported. The redesign is based on using the existing free-vortex type and solid-body type bladings, and the newly designed symmetrical blading. (Author)
- Language
- eng
- Extent
- 1 online resource (60 pages
- Note
-
- Title from cover
- "December 1973"--Cover
- "NPS-57VA73121A"--Cover
- Progress report to July 1973
- Author(s) subject terms: Axial compressor test rig, inlet throttle, flow measuring nozzles
- Label
- Redesign of the low speed three stage axial flow compressor test facility
- Title
- Redesign of the low speed three stage axial flow compressor test facility
- Statement of responsibility
- by M.H. Vavra, P.F. Pucci [and] W. Schlachter
- Language
- eng
- Summary
- A flow configuration of an existing low-speed, axial flow compressor test facility at the Turbopropulsion Laboratory, Naval Postgarduate School, Monterey, California, was redesigned in order to improve compressor inlet velocity distribution, improve mass flow measurement, and increase the power input. The design of the new configuration, consisting of an inlet nozzle, ducting, throttling device upstream of the compressor, and a diffusor downstream of it, is reported. The redesign is based on using the existing free-vortex type and solid-body type bladings, and the newly designed symmetrical blading. (Author)
- Cataloging source
- AD#
- http://library.link/vocab/creatorName
- Vavra, Michael Hans
- Government publication
- federal national government publication
- Illustrations
- illustrations
- Index
- no index present
- Literary form
- non fiction
- Nature of contents
-
- dictionaries
- bibliography
- technical reports
- http://library.link/vocab/relatedWorkOrContributorName
-
- Pucci, Paul F
- Schlachter, Wolfgang
- Naval Postgraduate School (U.S.)
- http://library.link/vocab/subjectName
-
- Compressors
- Compressors
- Naval Postgraduate School (U.S.)
- Type of report
- Technical report; 1973
- Label
- Redesign of the low speed three stage axial flow compressor test facility, by M.H. Vavra, P.F. Pucci [and] W. Schlachter
- Note
-
- Title from cover
- "December 1973"--Cover
- "NPS-57VA73121A"--Cover
- Progress report to July 1973
- Author(s) subject terms: Axial compressor test rig, inlet throttle, flow measuring nozzles
- Bibliography note
- Includes bibliographical references (p. 31-32)
- Color
- black and white
- Dimensions
- unknown
- Extent
- 1 online resource (60 pages
- Form of item
- online
- Governing access note
- "Approved for public release; distribution unlimited"--Cover
- Other physical details
- illustrations)
- Specific material designation
- remote
- Label
- Redesign of the low speed three stage axial flow compressor test facility, by M.H. Vavra, P.F. Pucci [and] W. Schlachter
- Note
-
- Title from cover
- "December 1973"--Cover
- "NPS-57VA73121A"--Cover
- Progress report to July 1973
- Author(s) subject terms: Axial compressor test rig, inlet throttle, flow measuring nozzles
- Bibliography note
- Includes bibliographical references (p. 31-32)
- Color
- black and white
- Dimensions
- unknown
- Extent
- 1 online resource (60 pages
- Form of item
- online
- Governing access note
- "Approved for public release; distribution unlimited"--Cover
- Other physical details
- illustrations)
- Specific material designation
- remote
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.archive.org/portal/Redesign-of-the-low-speed-three-stage-axial-flow/Ln-jvQBYDH4/" typeof="Book http://bibfra.me/vocab/lite/Item"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.archive.org/portal/Redesign-of-the-low-speed-three-stage-axial-flow/Ln-jvQBYDH4/">Redesign of the low speed three stage axial flow compressor test facility, by M.H. Vavra, P.F. Pucci [and] W. Schlachter</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.archive.org/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.archive.org/">Internet Archive - Open Library</a></span></span></span></span></div>
