Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Vavra, M.H."'
Experimental data are presented for the tangential and radial stresses in the disks of the 36,000 horsepower, 4000 rpm turbine for the M-1 engine oxidizer turbopump. The two-stage Curtis turbine is a special light-weight design utilizing thin conical
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::acf46fac55252e6542a99f2be8d54ba4
https://hdl.handle.net/10945/60068
https://hdl.handle.net/10945/60068
Autor:
Kenney, Paul Stephen, Vavra, M.H.
In this study, turbulent flow in a curved channel of square cross section was investigated experimentally to determine secondary flow effects. Probe surveys were conducted to establish vortex and total pressure loss distribution in the exit plane of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::7e209b49c12c1434081bb9cb48346e44
https://hdl.handle.net/10945/16671
https://hdl.handle.net/10945/16671
Akademický článek
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Akademický článek
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Autor:
Kelly, Robert Joseph
This work was undertaken to determine the pressure drops in the oxidizer flow passages of a compact dual-combustion liquid rocket engine by means of fluid dynamic model tests, using air instead of liquids, to establish design data. Investigated also
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::a2678cf38d49f74059b97cef444c10c8
https://hdl.handle.net/10945/12458
https://hdl.handle.net/10945/12458
Autor:
Riley, Michael William
This study was conducted to establish the performance parameters of a radial in-flow, dual discharge turbine and to determine the effect of axial clearance on these parameters. The results of the tests can be utilized for design improvements and for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::d7727cb3bae4514c01dbab6253b2d78f
https://hdl.handle.net/10945/43296
https://hdl.handle.net/10945/43296
Autor:
Wallace, Michael Walter
A series of air tests with two different turbines was carried out on the Turbine Test Rig at the Naval Postgraduate School, Monterey, California. This study is primarily concerned with the data reduction and performance analysis of these turbines. Re
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::4d5c2a06f520deb63c0810ffb9c90661
https://hdl.handle.net/10945/9606
https://hdl.handle.net/10945/9606
Autor:
Gallo, Salvatore Frank
This work was undertaken to check the feasibility of obtaining the velocity profiles downstream of the rotors of turbomachines by measuring only the radial distributions of total temperature, total pressure, and absolute flow angle and using these da
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::5b8854488e5f1c89bff09a7ad1278866
https://hdl.handle.net/10945/11806
https://hdl.handle.net/10945/11806
Autor:
Harrison, Robert Glen
http://archive.org/details/annalysisofsingl1094511635 Lieutenant, United States Navy
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::d46201ca50a8e4d056fc88f2f4a4da27
https://hdl.handle.net/10945/11635
https://hdl.handle.net/10945/11635
Autor:
Gapp, Donald Robert
This study presents the derivation of a diffuser design parameter, which takes into account losses due to the geometry of the diffuser. A criterion for design of annular diffusers, using the design parameter to predict losses, is developed from refer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::23807157b6f57409b0ef7eefcff2721d
https://hdl.handle.net/10945/14945
https://hdl.handle.net/10945/14945