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Terminal Shock And Restart Control Of A Mach 25 Axisymmetric Mixed Compression Inlet With 40 Percent Internal Contraction
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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 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 with total page 994 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Mach 2.5 Performance of a Bicone Inlet with Internal Focused Compression and 40 Percent Internal Contraction by : David A. Choby
Download or read book Mach 2.5 Performance of a Bicone Inlet with Internal Focused Compression and 40 Percent Internal Contraction written by David A. Choby and published by . This book was released on 1971 with total page 68 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 1974 with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Digital-computer Normal-shock-position and Restart Control of a Mach 2.5 Axisymmetric Mixed-compression Inlet by : George H. Neiner
Download or read book Digital-computer Normal-shock-position and Restart Control of a Mach 2.5 Axisymmetric Mixed-compression Inlet written by George H. Neiner and published by . This book was released on 1972 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development Publisher : ISBN 13 : Total Pages :194 pages Book Rating :4.0/5 ( download)
Book Synopsis Distortion Induced Engine Instability by : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Download or read book Distortion Induced Engine Instability written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1974 with total page 194 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 Terminal-shock and Restart Control of a Mach 2.5, Mixed-compression Inlet Coupled to a Turbofan Engine by : Robert J. Baumbick
Download or read book Terminal-shock and Restart Control of a Mach 2.5, Mixed-compression Inlet Coupled to a Turbofan Engine written by Robert J. Baumbick and published by . This book was released on 1974 with total page 26 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 1974 with total page 348 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Terminal-shock and Restart Control of Mach 2.5, Mixed-compression Inlet Couplet to a Turbofan Engine by : Robert J. Baumbick
Download or read book Terminal-shock and Restart Control of Mach 2.5, Mixed-compression Inlet Couplet to a Turbofan Engine written by Robert J. Baumbick and published by . This book was released on 1974 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Government Reports Index written by and published by . This book was released on 1975 with total page 1096 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 Design of a Very-low-bleed Mach 2.5 Mixed-compression Inlet with 45 Percent Internal Contraction by : Joseph F. Wasserbauer
Download or read book Design of a Very-low-bleed Mach 2.5 Mixed-compression Inlet with 45 Percent Internal Contraction written by Joseph F. Wasserbauer and published by . This book was released on 1975 with total page 76 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 1974 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Performance and Control of a Mach 3.0, Two-dimensional, External-internal-compression Inlet by :
Download or read book Investigation of the Performance and Control of a Mach 3.0, Two-dimensional, External-internal-compression Inlet written by and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Analytical Investigation of Fast Normal Shock Position Controls for a Mach 2.5 Mixed-compression Inlet by : George H. Neiner
Download or read book Experimental and Analytical Investigation of Fast Normal Shock Position Controls for a Mach 2.5 Mixed-compression Inlet written by George H. Neiner and published by . This book was released on 1971 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Poppet Valve Control of Throat Stability Bypass to Increase Stable Airflow Range of a Mach 2.5. Inlet with 60 Percent Internal Contraction by : Glenn A. Mitchell
Download or read book Poppet Valve Control of Throat Stability Bypass to Increase Stable Airflow Range of a Mach 2.5. Inlet with 60 Percent Internal Contraction written by Glenn A. Mitchell and published by . This book was released on 1975 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: The throat of a Mach 2.5 inlet with a coldpipe termination was fitted with a stability-bypass system. System variations included several stability bypass entrance configurations. Poppet valves controlled the bypass airflow. The inlet stable airflow range achieved with each configuration was determined for both steady state conditions and internal pulse transients. Results are compared with those obtained without a stability bypass system. Transient results were also obtained for the inlet with a choke point at the diffuser exit and for the inlet with large and small stability bypass plenum volumes. Poppet valves at the stability bypass exit provided the inlet with a stable airflow range of 20 percent or greater at all static and transient conditions.
