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Transonic And Supersonic Test Of A Mach 265 Mixed Compression Axisymmetric Intake
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Book Synopsis Transonic and Supersonic Test of a Mach 2.65 Mixed-compression Axisymmetric Intake by : J. L. Koncsek
Download or read book Transonic and Supersonic Test of a Mach 2.65 Mixed-compression Axisymmetric Intake written by J. L. Koncsek and published by . This book was released on 1972 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Common System Concept and Substantiation Test for an Axisymmetric Mixed Compression Supersonic Inlet by : Kee Soon Chun
Download or read book A Common System Concept and Substantiation Test for an Axisymmetric Mixed Compression Supersonic Inlet written by Kee Soon Chun and published by . This book was released on 1968 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Dynamic Response of a Mach 2.5 Axisymmetric Inlet with Engine Or Cold Pipe and Utilizing 60 Percent Supersonic Internal Area Contraction by : Joseph F. Wasserbauer
Download or read book Dynamic Response of a Mach 2.5 Axisymmetric Inlet with Engine Or Cold Pipe and Utilizing 60 Percent Supersonic Internal Area Contraction written by Joseph F. Wasserbauer and published by . This book was released on 1969 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: Dynamic response of supersonic mixed compression inlet coupled to cold pipe or turbojet engine.
Book Synopsis Investigation of a Mixed Compression Axisymmetric Inlet at Mach Number 5.3 by : Eldon A. Latham
Download or read book Investigation of a Mixed Compression Axisymmetric Inlet at Mach Number 5.3 written by Eldon A. Latham and published by . This book was released on 1972 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Terminal-shock and Restart Control of a Mach 2.5, Axisymmetric, Mixed Compression Inlet with 40 Percent Internal Contraction by : Robert J. Baumbick
Download or read book Terminal-shock and Restart Control of a Mach 2.5, Axisymmetric, Mixed Compression Inlet with 40 Percent Internal Contraction written by Robert J. Baumbick and published by . This book was released on 1974 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results of experimental tests conducted on a supersonic, mixed-compression, axisymmetric inlet are presented. The inlet is designed for operation at Mach 2.5 with a turbofan engine (TF-30). The inlet was coupled to either a choked orifice plate or a long duct which had a variable-area choked exit plug. Closed-loop frequency responses of selected diffuser static pressures used in the terminal-shock control system are presented. Results are shown for Mach 2.5 conditions with the inlet coupled to either the choked orifice plate or the long duct. Inlet unstart-restart traces are also presented. High-response inlet bypass doors were used to generate an internal disturbance and also to achieve terminal-shock control.
Book Synopsis Mach 3 Wind Tunnel Test of Mixed Compression Supersonic Inlet by : Akira Murakami
Download or read book Mach 3 Wind Tunnel Test of Mixed Compression Supersonic Inlet written by Akira Murakami and published by . This book was released on 1992 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Performance of a Mach Number 3.0 Design Axisymmetric Double-cone External-compression Inlet in the Mach Number Range 1.97 to 0.79 by : Owen H. Davis
Download or read book Performance of a Mach Number 3.0 Design Axisymmetric Double-cone External-compression Inlet in the Mach Number Range 1.97 to 0.79 written by Owen H. Davis and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 1980 with total page 1280 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Numerical Investigation of Mach 2.5 Supersonic Mixed Compression Inlet by : Akira Fujimoto
Download or read book Experimental and Numerical Investigation of Mach 2.5 Supersonic Mixed Compression Inlet written by Akira Fujimoto and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Performance Summary and Analysis of a Mach 3.0 Design Axisymmetric All-external-compression Double-cone Inlet Mach Number Range 3.0 to 0.8 by : John L. Allen
Download or read book Performance Summary and Analysis of a Mach 3.0 Design Axisymmetric All-external-compression Double-cone Inlet Mach Number Range 3.0 to 0.8 written by John L. Allen and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Dynamic Response of a Two-dimensional, Mach 2.7, Mixed-compression Inlet by : Robert J. Baumbick
Download or read book Experimental Dynamic Response of a Two-dimensional, Mach 2.7, Mixed-compression Inlet written by Robert J. Baumbick and published by . This book was released on 1972 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: A test program was conducted on a two-dimensional supersonic inlet. Internal disturbances in diffuser exit mass flow were produced by oscillating overboard bypass doors. Open-loop dynamic responses of shock position, throat exit and diffuser exit static pressures are presented. The steady-state and dynamic coupling between ducts were also obtained. The experimental results from the two-dimensional inlet are compared to results from a similar size axisymmetric inlet and also to a transfer function synthesis program.
Book Synopsis Tolerance of Mach 2.50 Axisymmetric Mixed-compression Inlets to Upstream Flow Variations by : David A. Choby
Download or read book Tolerance of Mach 2.50 Axisymmetric Mixed-compression Inlets to Upstream Flow Variations written by David A. Choby and published by . This book was released on 1972 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Boundary Layers in an Axisymmetric Mach 2.5, Mixed Compression Inlet by : Warren R. Hingst
Download or read book Experimental Investigation of Boundary Layers in an Axisymmetric Mach 2.5, Mixed Compression Inlet written by Warren R. Hingst and published by . This book was released on 1973 with total page 33 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 1978 with total page 1308 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Analysis of Mach Number Variation Effect on a Two Dimensional Mixed Compression Supersonic Inlet Using CFD Simulation Through Parallel Computing by : Taher O. Fodeibou
Download or read book Analysis of Mach Number Variation Effect on a Two Dimensional Mixed Compression Supersonic Inlet Using CFD Simulation Through Parallel Computing written by Taher O. Fodeibou and published by . This book was released on 2009 with total page 188 pages. Available in PDF, EPUB and Kindle. Book excerpt: "The study focuses on the effect of Mach number variation on a mixed compression supersonic inlet."(i).
Book Synopsis Digital Integrated Control of a Mach 2.5 Mixed-compression Supersonic Inlet and an Augmented Mixed-flow Turbofan Engine by : Peter G. Batterton
Download or read book Digital Integrated Control of a Mach 2.5 Mixed-compression Supersonic Inlet and an Augmented Mixed-flow Turbofan Engine written by Peter G. Batterton and published by . This book was released on 1974 with total page 0 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 1992 with total page 1020 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)