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 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 Monthly Catalog of United States Government Publications Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1978 with total page 1300 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960-07 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Rocket armament Exhaust Gas on the Performance of a Supersonic inlet J34 turbojet engine Installation at Mach 2 0 written by Milton A. Beheim and published by . This book was released on 1956 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of the effects of rocket-armament-exhaust-gas ingestion on the performance of a supersonic-inlet J34-turbojet-engine installation was conducted at Mach 2.0. The increase in compressor-inlet temperature resulted in decreased corrected engine air flow and caused the inlet to operate at decreased mass-flow ratios. The inlet normal shock fluctuated rapidly during this disturbance, particularly when the inlet was forced to enter a region where buzz ordinarily occurred. Temperatures increased throughout the engine, and pressure generally decreased. Engine speed increased when the inlet temperature rise was large, but corrected engine speed decreased. Compressor pressure ratio remained essentially constant.

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 Scientific and Technical Aerospace Reports written by and published by . This book was released on 1963 with total page 1222 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 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 Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1960 with total page 450 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 Effects of Variable Turbine Area on Subsonic Cruise Performance of Turbojets Designed for Supersonic Application written by Arvid L. Keith and published by . This book was released on 1970 with total page 76 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 Supersonic Inlet engine Control Using Engine Speed as a Primary Variable for Controlling Normal Shock Position written by Francis J. Paulovich and published by . This book was released on 1971 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: A cross-coupled inlet-engine control system concept is presented for a supersonic propulsion system consisting of a mixed- compression inlet and a turbojet engine. The control system employs manipulation of both bypass door flow area and engine speed to stabilize normal shock position in the inlet. Specifically, the case of slow-acting bypass doors used as a reset control where engine speed is the primary means of shock position control is described. Experimental results are presented showing performance of the control system with a NASA-designed inlet and a turbojet engine operating at Mach 2.5 in the Lewis 10- by 10-Foot Supersonic Wind Tunnel.

Download or read book Inlet Sensitivity Study for a Supersonic Transport written by Robert W. Koenig and published by . This book was released on 1967 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effect of Heat and Power Extraction on Turbojet engine Performance written by Stanley L. Koutz and published by . This book was released on 1951 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: In general, with a turbojet engine operating at constant engine speed, bleeding gas from the tail pipe at constant tail-pipe-nozzle area and reduced turbine-inlet temperature caused 2.5 to 4 times as great a loss in thrust as bleeding gas at constant turbine-inlet temperature and reduced tail-pipe-nozzle area.

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1968 with total page 1312 pages. Available in PDF, EPUB and Kindle. Book excerpt: