Explore Books on
impellers
1-24 of 45 Books
Mixing equipment (impeller type)
Mixing equipment (impeller type)
By American Institute of Chemical Engineers. Equipment Testing Procedures Committee.
Detailed flow measurements in casing boundary layer of 427-meter-per-second-tip-speed two-stage fan with casing treatment
Detailed flow measurements in casing boundary layer of 427-meter-per-second-tip-speed two-stage fan with casing treatment
By William T. Gorrell
A finite-element-based perturbation model for the rotordynamic analysis of shrouded pump impellers
A finite-element-based perturbation model for the rotordynamic analysis of shrouded pump impellers
By Eriane A. Baskharone
Detailed flow measurements in casing boundary layer of 429-meter-per-second-tip-speed two-stage fan
Detailed flow measurements in casing boundary layer of 429-meter-per-second-tip-speed two-stage fan
By William T. Gorrell
Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row
Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row
By Charles A. Farrell
A prediction of 3-D viscous flow and performance of the NASA low-speed centrifugal compressor
A prediction of 3-D viscous flow and performance of the NASA low-speed centrifugal compressor
By John Moore
Analytic investigation of effect of end-wall contouring on stator performance
Analytic investigation of effect of end-wall contouring on stator performance
By Robert J. Boyle
Prochnostʹ ėlementov rotorov turbomashin
Prochnostʹ ėlementov rotorov turbomashin
By Respublikanskiĭ nauchno-tekhnicheskiĭ seminar "Prochnostʹ ėlementov rotorov turbomashin" (2nd 1978 Kiev, Ukraine)
Avtomaticheskoe uravnoveshivanie rotorov bystrokhodnykh mashin
Avtomaticheskoe uravnoveshivanie rotorov bystrokhodnykh mashin
By Anatoliĭ Aleksandrovich Kuindzhi
Horsepower tables for agitator impellers
By L. T. Advani
Simplified design theory for highly loaded axial compressor rotors and experimental study of two transonic examples
Simplified design theory for highly loaded axial compressor rotors and experimental study of two transonic examples
By Arthur John Wennerstrom
Rotordynamic instability problems in high-performance turbomachinery, 1988
Rotordynamic instability problems in high-performance turbomachinery, 1988
By
Rotordynamic instability problems in high-performance turbomachinery, 1986
Rotordynamic instability problems in high-performance turbomachinery, 1986
By
Rotordynamic instability problems in high-performance turbomachinery, 1984
Rotordynamic instability problems in high-performance turbomachinery, 1984
By
Rotordynamic instability problems in high-performance turbomachinery 1993
Rotordynamic instability problems in high-performance turbomachinery 1993
By United States. National Aeronautics and Space Administration.
Structural dynamic aspects of bladed disk assemblies
Structural dynamic aspects of bladed disk assemblies
By A. V. Srinivasan
Prochnostʹ rabochikh koles turbomashin
Prochnostʹ rabochikh koles turbomashin
By I. A. Kozlov,Georgiĭ Stepanovich Pisarenko
Analytic investigation of effect of end-wall contouring on stator performance
Analytic investigation of effect of end-wall contouring on stator performance
By Robert J. Boyle
Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impeller
Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impeller
By Lawrence F. Schumann
Eine einfache halbgraphische Methode für die Formulierung der Funktion Ne=f(Re) in der Rührtechnik aus dem bekannten Graph
Eine einfache halbgraphische Methode für die Formulierung der Funktion Ne=f(Re) in der Rührtechnik aus dem bekannten Graph
By Jouko Laine
Rotordynamic instability problems in high-performance turbomachinery - 1982
Rotordynamic instability problems in high-performance turbomachinery - 1982
By United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Rotordynamic instability problems in high-performance turbomachinery
Rotordynamic instability problems in high-performance turbomachinery
By United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch