Download or read book Dynamics of a Supersonic Inlet with Adjustable Bypass in Combination with a J34 Turbojet Engine written by Fred Allen Wilcox and published by . This book was released on 1956 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Dynamic Response of a Supersonic Diffuser to Bypass and Spike Oscillation written by David N. Bowditch and published by . This book was released on 1959 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of a Continuous Normal shock Positioning Control on the Bypass of a Supersonic Inlet in Combination with the J34 Turbojet Engine written by Fred A. Wilcox and published by . This book was released on 1956 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt: A normal-shock positioning control which utilized the bypass of a supersonic inlet to set the required air flow for a J34 turbojet engine was investigated to Mach number 2.0 in the Lewis 8- by 6-foot supersonic tunnel. A small static probe extending from the cowl was used to position the normal shock slightly ahead of the cowl lip and gave subcritical inlet operation. Continuous control was provided through a hydraulic servoactuator.
Download or read book Effect of an Adjustable Supersonic Inlet on the Performance Up to Mach Number 2 0 of a J34 Turbojet Engine written by Andrew Beke and published by . This book was released on 1956 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Adjustable Supersonic Inlet in Combination with J34 Engine Up to Mach 2 0 written by J.C. Nettles and published by . This book was released on 1954 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Dynamics of a Supersonic Inlet engine Combination Subjected to Disturbances in Fuel Flow and Inlet Overboard Bypass Airflow written by Robert E. Wallhagen and published by . This book was released on 1972 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Monthly Catalog of United States Government Publications written by United States. Superintendent of Documents and published by . This book was released on 1960 with total page 1812 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Cumulative Title Index to United States Public Documents 1789 1976 written by Daniel W. Lester and published by . This book was released on 1980 with total page 562 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Performance of a Turbojet Engine in Combination with an External internal compression Inlet to Mach 2 88 written by David N. Bowditch and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Contractor Report written by United States. National Aeronautics and Space Administration and published by . This book was released on 1970 with total page 1008 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1980 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Steady state Interactions from Mach 1 98 to 2 58 Between a Turbojet Engine and an Axisymmetric Inlet with 60 percent Internal Area Contraction written by David A. Choby and published by . This book was released on 1969 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Fixed geometry Supersonic Inlets with Bypass Ducts for Matching Turbojet engine Air flow Requirements Over a Range of Transonic and Supersonic Speeds written by Abraham Leiss and published by . This book was released on 1958 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is presented to design a supersonic inlet that will match turbojet-engine air mass-flow requirements over a wide Mach number range. Two types of bypasses were investigated; one had a 360 degree annular cowling and the other had twin slotted ducts. Three models were flight tested. Two of the models, which had bypass ducts, were also ground tested. The bypass models had higher external drags. Both bypass models approximated a typical turbojet-engine air mass-flow requirement between Mach numbers 1.0 and 2.0. The flight tests covered a Reynolds number range from 200,000 to 800,000 and a Mach number range from 0.8 to 1.95.
Download or read book A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft written by Clifford J. Moore and published by . This book was released on 1970 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report investigates critical reviews of NACA and NASA report literature on light aircraft design, with emphasis on propulsion subsystems, stability, control, propellers, performance, and safety.
Download or read book NASA Technical Note written by and published by . This book was released on 1971 with total page 304 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Index of NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960 with total page 448 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft Volume 3 Propulsion Subsystems Performance Stability and Control Propellers and Flight Safety written by Clifford J. Moore and published by . This book was released on 1970 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt:
