Download or read book Flow Fluctuations and Alternating Blade Stresses in a Single stage Compressor written by R. Chaplin and published by . This book was released on 1958 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flow Fluctuations and Alternating Blade Stresses in the First Stage of an Axial Compressor written by T. J. Hargest and published by . This book was released on 1953 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Current Papers written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1961 with total page 782 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Alternating Pressures and Blade Stresses in an Axial Flow Compressor written by J. R. Forshaw and published by . This book was released on 1951 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1962 with total page 1116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Alternating Pressures and blade stresses in an axial flow compressor written by J. R. Forshaw and published by . This book was released on 1956 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Boundary Layer and Wake Modifications to Compressor Design Systems written by Arun K. Sehra and published by . This book was released on 1979 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effect of blade-to-blade flow variations on the mean flow field of a highly loaded transonic axial flow compressor was invesitaged. The theoretical approach centered around modeling of three important phenomena associated with blade-to-blade flow fluctuations, which control the mean momentum and energy transfer processes. Apparent stresses were introduced into the mean flow momentum equations by pitchwise averaging. Loss concept of mean relative total pressure, due to conversion of mean flow kinetic energy to the energy of fluctuations, was introduced. Based on this concept, mean rothalpy and the production of apparent entropy were defined. An expression for mean rothalpy variation along the streamline was derived by pitchwise averaging of the energy equation. Mean flow equations suitable for the streamline curvature computational scheme were developed which include these three effects. Apparent stresses, mean rothalpy and apparent entropy variations were calculated from measured velocity fluctuations. The revised streamline curvature procedure was then used to predict the axisymmetric (peripheral mean) flow. The agreement of rotor outlet tangential velocity is excellent reproducing an unusual peak which is not explainable by usual techniques. The results showed that 3-D inviscid effects do not significantly modify the mean flow, and that the direct effect of apparent stresses on the mean flow is also small.

Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1962 with total page 914 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Journal of the Royal Aeronautical Society written by Royal Aeronautical Society and published by . This book was released on 1962 with total page 1164 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Technical Publications Announcements written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960 with total page 448 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Strain Gage Readings written by and published by . This book was released on 1962 with total page 754 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Vibration Survey of Blades in 10 stage Axial flow Compressor written by Andre J. Meyer (Jr.) and published by . This book was released on 1949 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of the High Alternating Stresses in the Blades of an Axial flow Compressor written by Aeronautical Research Council and published by . This book was released on 1957 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of the High Alternating Stresses in the Blades of an Axial flow Compressor written by Aeronautical Research Council and published by . This book was released on 1957 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Thesis written by and published by . This book was released on 1962 with total page 586 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Some Effects of Blade Trailing edge Thickness on Performance of a Single stage Axial flow Compressor written by J. J. Moses and published by . This book was released on 1951 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Pressure distribution Measurements on the Rotating Blades of a Single stage Axial flow Compressor written by Jack F. Runckel and published by . This book was released on 1947 with total page 550 pages. Available in PDF, EPUB and Kindle. Book excerpt: A preliminary investigation has been made of the pressure distribution about the mean-radius section of the rotating blades of a single-stage axial-flow compressor at a blade Mach number of 0.35. A 24-cell pressure-transfer device used in obtaining the pressure data is described and the accuracy of these data is established by several independent methods.