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Internal Flow Characteristics Of A Multistage Compressor With Inlet Pressure Distortion J85 13 Turbojet Engine Studies
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781725989283 Total Pages :42 pages Book Rating :4.9/5 (892 download)
Book Synopsis Internal Flow Characteristics of a Multistage Compressor with Inlet Pressure Distortion. [j85-13 Turbojet Engine Studies] by : National Aeronautics and Space Administration (NASA)
Download or read book Internal Flow Characteristics of a Multistage Compressor with Inlet Pressure Distortion. [j85-13 Turbojet Engine Studies] written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-22 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: The measured distribution of compressor interstage pressures and temperatures resulting from a 180 deg inlet-total-pressure distortion for a J85-13 turbojet engine is reported. Extensive inner stage instrumentation combined with stepwise rotation of the inlet distortion gave data of high circumferential resolution. The steady-state pressures and temperatures along with the amplitude, extent, and location of the distorted areas are given. Data for 80, 90, and 100 percent of rotor design speed are compared with clean (undistorted) inlet flow conditions to show pressure and temperature behavior within the compressor. Both overall and stagewise compressor performances vary only slightly when clean and distorted inlet conditions are compared. Total and static pressure distortions increase in amplitude in the first few stages of the compressor and then attenuate fairly uniformly to zero at the discharge. Total-temperature distortion induced by the pressure distortion reached a maximum amplitude by the first two stages and decayed only a little through the rest of the compressor. Distortion amplitude tended to peak in line with the screen edges, and, except for total and static pressure in the tip zone, there was little swirl in the axial direction. Debogdan, C. E. and Moss, J. E., Jr. and Braithwaite, W. M. Glenn Research Center NASA-TM-X-3446, E-8848 RTOP 505-05...
Book Synopsis Internal Flow Characteristics of a Multistage Compressor with Inlet Pressure Distortion by : Claude E. DeBogdan
Download or read book Internal Flow Characteristics of a Multistage Compressor with Inlet Pressure Distortion written by Claude E. DeBogdan and published by . This book was released on 1977 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Analysis of Internal Flow of J85-13 Multistage Compressor by : Roy D. Hager
Download or read book Analysis of Internal Flow of J85-13 Multistage Compressor written by Roy D. Hager and published by . This book was released on 1977 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Performance of a J85-13 Compressor with Clean and Distorted Inlet Flow by : Edward J. Milner
Download or read book Performance of a J85-13 Compressor with Clean and Distorted Inlet Flow written by Edward J. Milner and published by . This book was released on 1975 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results presented are of a series of experimental tests in which a J85-13 turbojet engine was subjected to both distorted and undistorted inlet total pressure conditions. A distinctive feature of the data base obtained is that it includes compressor interstage information not previously recorded for a J85-13 engine. Each of the eight compressor stages was instrumented to obtain the characteristics of the individual stages for undistorted inlet conditions, and these data are documented in the report along with the undistorted compressor overall performance. Also included in the report is the overall performance of the compressor exposed to 14 different distorted-inlet conditions - 10 circumferential patterns and 4 radial patterns. The distortion patterns were introduced using screens that spoiled from 8 to 50 percent of the compressor face area; the distortion screen density, or the area blocked by the screen wire per unit area of screen, varied from 26 to 69 percent.
Book Synopsis Internal Flow Characteristics of a Multistage Compressor with Inlet Pressure Distortion by : Claude E. DeBogdan
Download or read book Internal Flow Characteristics of a Multistage Compressor with Inlet Pressure Distortion written by Claude E. DeBogdan and published by . This book was released on 1977 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1978 with total page 356 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Bibliography of Lewis Research Center Technical Publications Announced in 1977 by : Lewis Research Center
Download or read book Bibliography of Lewis Research Center Technical Publications Announced in 1977 written by Lewis Research Center and published by . This book was released on 1978 with total page 356 pages. Available in PDF, EPUB and Kindle. Book excerpt: This compilation of abstracts describes and indexes over 780 technical reports resulting from the scientific and engineering work performed and managed by the Lewis Research Center in 1977. All the publications were announced in the 1977 issues of STAR (Scientific and Technical Aerospace Reports) and/or IAA (International Aerospace Abstracts). Documents cited include research reports, journal articles, conference presentations, patents and patent applications, and theses.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1985 with total page 1346 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781724242174 Total Pages :32 pages Book Rating :4.2/5 (421 download)
Book Synopsis Analytical Prediction of the Performance and Stability of a J85-13 Compressor with Distorted Inlet Flow by : National Aeronautics and Space Administration (NASA)
Download or read book Analytical Prediction of the Performance and Stability of a J85-13 Compressor with Distorted Inlet Flow written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-25 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: The parallel compressor concept was studied using a compressor model based on the overall clean-inlet performance map obtained from experimental tests in an altitude chamber using a General Electric J85-13 turbojet engine. The model, which includes a static-pressure balance calculation at compressor discharge, was exercised at conditions corresponding to 10 different screen-induced distortion patterns included in the experimental data base. The spoiled area of these patterns ranged from 30 deg to 180 deg, and the distortion screen density, or the area blocked by the screen wire per unit area of screen, varied from 26 to 69 percent. The study indicates that at the higher corrected speeds, the analytical surge lines obtained are good representations of the corresponding experimental surge lines and are independent of distortion angle or distortion angle or distortion level. Milner, E. J. Glenn Research Center NASA-TM-X-3515, E-8887 RTOP 505-05
Book Synopsis Analytical Prediction of the Performance and Stability of a J85-13 Compressor with Distorted Inlet Flow by : Edward J. Milner
Download or read book Analytical Prediction of the Performance and Stability of a J85-13 Compressor with Distorted Inlet Flow written by Edward J. Milner and published by . This book was released on 1977 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: The parallel compressor concept was studied using a compressor model based on the overall clean-inlet performance map obtained from experimental tests in an altitude chamber using a General Electric J85-13 turbojet engine. The model, which includes a static-pressure balance calculation at compressor discharge, was exercised at conditions corresponding to 10 different screen-induced distortion patterns included in the experimental data base. The spoiled area of these patterns ranged from 30 deg to 180 deg, and the distortion screen density, or the area blocked by the screen wire per unit area of screen, varied from 26 to 69 percent. The study indicates that at the higher corrected speeds, the analytical surge lines obtained are good representations of the corresponding experimental surge lines and are independent of distortion angle or distortion angle or distortion level.
Download or read book NASA SP. written by and published by . This book was released on 1978 with total page 654 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aeronautical Engineering written by and published by . This book was released on 1978 with total page 644 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Book Synopsis Steady-state Interactions from Mach 1.98 to 2.58 Between a Turbojet Engine and an Axisymmetric Inlet with 60-percent Internal Area Contraction by : David A. Choby
Download or read book Steady-state Interactions from Mach 1.98 to 2.58 Between a Turbojet Engine and an Axisymmetric Inlet with 60-percent Internal Area Contraction written by David A. Choby and published by . This book was released on 1969 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Circumferential Total-pressure Gradients Typical of Single-inlet Duct Installations on Performance of an Axial-flow Turbojet Engine by : S. C. Huntley
Download or read book Effect of Circumferential Total-pressure Gradients Typical of Single-inlet Duct Installations on Performance of an Axial-flow Turbojet Engine written by S. C. Huntley and published by . This book was released on 1955 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1971 with total page 1388 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Frequency Response of an Axial-flow Compressor Exposed to Inlet Pressure Perturbations by : Edward J. Milner
Download or read book Frequency Response of an Axial-flow Compressor Exposed to Inlet Pressure Perturbations written by Edward J. Milner and published by . This book was released on 1974 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications, Cumulative Index by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications, Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1976 with total page 1408 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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