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Analysis And Testing Of Two Dimensional Vented Coanda Ejectors With Asymmetric Variable Area Mixing Sections
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Book Synopsis Analysis and Testing of Two-dimensional Vented Coanda Ejectors with Asymmetric Variable Area Mixing Sections by :
Download or read book Analysis and Testing of Two-dimensional Vented Coanda Ejectors with Asymmetric Variable Area Mixing Sections written by and published by . This book was released on 1976 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Analysis and Testing of Two-dimensional Vented Coanda Ejectors with Asymmetric Variable Area Mixing Sections by : Dynatech Corporation
Download or read book Analysis and Testing of Two-dimensional Vented Coanda Ejectors with Asymmetric Variable Area Mixing Sections written by Dynatech Corporation and published by . This book was released on 1976 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Analysis and Testing of Two-dimensional Slot Nozzle Ejectors with Variable Area Mixing Sections by : Gerald B. Gilbert
Download or read book Analysis and Testing of Two-dimensional Slot Nozzle Ejectors with Variable Area Mixing Sections written by Gerald B. Gilbert and published by . This book was released on 1973 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt: Finite difference computer techniques have been used to calculate the detailed performance of air to air two-dimensional ejectors with symmetric variable area mixing sections and coaxial coverging primary nozzles. The analysis of the primary nozzle assumed correct expansion of the flow and is suitable for subsonic and slightly supersonic velocity levels. The variation of the mixing section channel walls is assumed to be gradual so that the static pressure can be assumed uniform on planes perpendicular to the axis. A test program was run to provide two-dimensional ejector test data for verification of the computer analysis. A primary converging nozzle with a discharge geometry of 0.125 inch x 8.0 inch was supplied with 600 SCFM of air at about 35 psia and 180 F. This nozzle was combined with two mixing section geometries with throat sizes of 1.25 inch x 8.0 inch and 1.875 inch x 8.0 inch and was tested at a total of 11 operating points.
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 1977 with total page 1160 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Thrust Augmentor Application for STOL and V/STOL by :
Download or read book Thrust Augmentor Application for STOL and V/STOL written by and published by . This book was released on 1977 with total page 20 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 1977 with total page 1746 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalogue, United States Public Documents by :
Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1977 with total page 1724 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government reports annual index by :
Download or read book Government reports annual index written by and published by . This book was released on 199? with total page 908 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Collection of Technical Papers by :
Download or read book A Collection of Technical Papers written by and published by . This book was released on 1981 with total page 764 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Contractor Report written by and published by . This book was released on 1976 with total page 676 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Aeronautical Journal written by and published by . This book was released on 1977 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Ames Research Center Publications-1976 by :
Download or read book Ames Research Center Publications-1976 written by and published by . This book was released on 1978 with total page 178 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Announcements & Index by :
Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1977-03 with total page 1430 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Analysis of the Properties of Two-dimensional Incompressible Fluid Flow in the Mixing Chamber of a Constant Area Ejector by : Martin D. Kiefer
Download or read book An Analysis of the Properties of Two-dimensional Incompressible Fluid Flow in the Mixing Chamber of a Constant Area Ejector written by Martin D. Kiefer and published by . This book was released on 1963 with total page 85 pages. Available in PDF, EPUB and Kindle. Book excerpt: The properties of an incompressible fluid in the mixing chamber of a constant area cylindrical ejector are analyzed in a two-dimensional form. The flow field for velocity and temperature is assumed to be made up of regions in which uniform flow of the primary and secondary fluids exist, and which diminish with axial distance from the ejector entrance. The velocity and temperature distributions in the mixed region are assumed to have cosine shaped profiles. The compatible solutions are given an axial distribution by assuming a parabolic spread rate for the secondary fluid jet boundary. Results are generated in the form of a non-dimensional velocity and pressure, a normalized temperature and a Momentum Factor, as functions of axial distance.
Book Synopsis Investigation of the Mixing Region Between the Primary and Secondary Streams of a Twodimensional Supersonic Air-air Ejector System by : James R. Nelson
Download or read book Investigation of the Mixing Region Between the Primary and Secondary Streams of a Twodimensional Supersonic Air-air Ejector System written by James R. Nelson and published by . This book was released on 1965 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt: The turbulent mixing region of a two-dimensional, supersonic, air-air ejector system was experimentally investigated utilizing an interferometer. Density distributions for the two-stream mixing region within the ejector duct were established for 6 different test configurations. Similarity of the density distributions was indicated for mixing region cross sections as close as one nozzleexit hydraulic diameter from the nozzle. Density profiles at successive downstream duct locations were plotted to show the spread of the mixing region. The effect of normal and oblique shocks on the rate of spread of the mixing region was found to be small. In addition, ejector performance data and techniques for spark lamp photography are presented. It is concluded that the interferometer could be effectively utilized to help determine the transport coefficients of ejector system turbulent mixing processes. (Author).
Book Synopsis An Analysis of the Properties of Two-dimensional Incompressible Fluid Flow in the Mixing Chamber of a Constant Area Ejector by :
Download or read book An Analysis of the Properties of Two-dimensional Incompressible Fluid Flow in the Mixing Chamber of a Constant Area Ejector written by and published by . This book was released on 1963 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The properties of an incompressible fluid in the mixing chamber of a constant area cylindrical ejector are analyzed in a two-dimensional form. The flow field for velocity and temperature is assumed to be made up of regions in which uniform flow of the primary and secondary fluids exist, and which diminish with axial distance from the ejector entrance. The velocity and temperature distributions in the mixed region are assumed to have cosine shaped profiles. The compatible solutions are given an axial distribution by assuming a parabolic spread rate for the secondary fluid jet boundary. Results are generated in the form of a non-dimensional velocity and pressure, a normalized temperature and a Momentum Factor, as functions of axial distance.
Book Synopsis Understanding Aerospace Chemical Propulsion by : H. S. Mukunda
Download or read book Understanding Aerospace Chemical Propulsion written by H. S. Mukunda and published by . This book was released on 2017-02-28 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Explores aeronautical and space chemical propulsion. The book provides an understanding of propulsion systems through illustrative description of the systems; analysis of modeled systems; examination of the performance of real systems in this light; and a comparative assessment of aeronautical and space propulsion system elements.