Download or read book Distributed Educated Throat Stability Bypass to Increase the Stable Airflow Range of a Mach 2 5 Inlet with 60 percent Internal Contraction written by Robert Joseph Shaw and published by . This book was released on 1974 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of an experimental investigation to increase the stable airflow operating range of a supersonic mixed-compression inlet are presented. A distributed educated throat stability-bypass entrance configuration was tested. In terms of diffuser-exit corrected airflow, a large inlet stable airflow range of about 16.1 percent was obtained if a constant pressure was maintained in the bypass plenum. Limited unstart angle of attack data are presented.
Download or read book Throat Stability bypass Systems to Increase the 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 1974 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Distributed Porous Throat Stability Bypass to Increase the Stable Airflow Range of a Mach 2 5 Inlet with 60 Percent Internal Contraction written by Robert Joseph Shaw and published by . This book was released on 1974 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of an experimental investigation to increase the stable airflow operating range of a supersonic, mixed-compression inlet with 60-percent internal contraction are presented. Various distributed-porous, throat stability-bypass entrance configurations were tested. In terms of diffuser-exit corrected airflow, a large inlet stable airflow range of about 25 percent was obtained with the optimum configuration if a constant pressure was maintained in the by-pass plenum. The location of the centerbody bleed region had a decided effect on the overall inlet performance. Limited unstart angle-of-attack data are presented.
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1975 with total page 1080 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1980 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by United States. National Aeronautics and Space Administration and published by . This book was released on 1980 with total page 922 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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.
Download or read book Dynamic Response of a Mach 2 5 Axisymmetric Inlet and Turbojet Engine with a Poppet value Controlled Inlet Stability Bypass System when Subjected to Internal and External Airflow Transients written by and published by . This book was released on 1980 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Dynamic Response of a Mach 2 5 Axisymmetric Inlet and Turbojet Engine with a Poppet valve controlled Inlet stability Bypass System when Subjected to Internal and External Airflow Transients written by Bobby W. Sanders and published by . This book was released on 1980 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1974 with total page 960 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Download or read book Forward slanted Slot Throat Stability Bypass to Increase the Stable Airflow Range of a Mach 2 5 Inlet with 60 percent Internal Contraction written by Robert Joseph Shaw and published by . This book was released on 1974 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Turbojet exhaust nozzle Secondary airflow Pumping as an Exit Control of an Inlet stability Bypass System for a Mach 2 5 Axisymmetric Mixed compression Inlet written by Bobby W. Sanders and published by . This book was released on 1980 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Distributed Porous Throat Stability Bypass to Increase the Stable Airflow Range of a Mach 2 5 Inlet with 60 Percent Internal Contraction written by Robert Joseph Shaw and published by . This book was released on 1974 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of an experimental investigation to increase the stable airflow operating range of a supersonic, mixed-compression inlet with 60-percent internal contraction are presented. Various distributed-porous, throat stability-bypass entrance configurations were tested. In terms of diffuser-exit corrected airflow, a large inlet stable airflow range of about 25 percent was obtained with the optimum configuration if a constant pressure was maintained in the by-pass plenum. The location of the centerbody bleed region had a decided effect on the overall inlet performance. Limited unstart angle-of-attack data are presented.
Download or read book Pressure activated Stability bypass control Valves to Increase the Stable Airflow Range of a Mach 2 5 Inlet with 40 Percent Internal Contraction written by Glenn A. Mitchell and published by . This book was released on 1974 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Government Reports Annual Index written by and published by . This book was released on 1974 with total page 900 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 908 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Experimental Investigation of Forced Mixing of a Turbulent Boundary Layer in an Annular Diffuser written by Robert Joseph Shaw and published by . This book was released on 1981 with total page 378 pages. Available in PDF, EPUB and Kindle. Book excerpt:
