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Author : J. L. Koncsek
Publisher :
ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.:/5 (31 download)
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 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Joseph F. Wasserbauer
Publisher :
ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.:/5 (31 download)
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.
Author : Kee Soon Chun
Publisher :
ISBN 13 :
Total Pages : 9 pages
Book Rating : 4.:/5 (455 download)
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:
Author : Robert J. Baumbick
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (31 download)
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.
Author : Eldon A. Latham
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)
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:
Author : Akira Murakami
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
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:
Author : Owen H. Davis
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (317 download)
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:
Author :
Publisher :
ISBN 13 :
Total Pages : 1280 pages
Book Rating : 4.:/5 (31 download)
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:
Author : John L. Allen
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (31 download)
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:
Author : Akira Fujimoto
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
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:
Author : Robert J. Baumbick
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)
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.
Author : David A. Choby
Publisher :
ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (486 download)
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:
Author : Warren R. Hingst
Publisher :
ISBN 13 :
Total Pages : 33 pages
Book Rating : 4.:/5 (11 download)
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:
Author : Sudip Das
Publisher : LAP Lambert Academic Publishing
ISBN 13 : 9783659284939
Total Pages : 344 pages
Book Rating : 4.2/5 (849 download)
Download or read book Studies on a Rectangular Mixed Compression Supersonic Air-Intake written by Sudip Das and published by LAP Lambert Academic Publishing. This book was released on 2012 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt: Computational and experimental studies have been carried out, on a rectangular mixed compression supersonic air-intake designed for Mach 2.2. The details of flow field have been obtained with different cowl deflection angles and back pressures. The effectiveness of cowl deflection compared to conventional bleed has been investigated. Unsteady flow field details inside the intake duct with cowl deflection and back pressure have been also obtained. The study provides the start / unstart characteristics of intake with bleed and cowl deflection angle, performance with combined adoption of bleed and cowl deflection together, the effect of cowl deflection angle without and with various back pressures and the unsteady flow field characteristics inside the intake duct. These studies give the details of complex flow existing inside the air-intake even at design conditions and the possibility of adopting cowl deflection to improve the performance of intakes. The details obtained from the present study are expected to provide useful inputs towards the design of air-intakes at supersonic speed.
Author :
Publisher :
ISBN 13 :
Total Pages : 1308 pages
Book Rating : 4.:/5 (3 download)
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:
Author : Taher O. Fodeibou
Publisher :
ISBN 13 :
Total Pages : 188 pages
Book Rating : 4.:/5 (457 download)
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).
Author : Peter G. Batterton
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (689 download)
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:
