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Preliminary Analysis Of Supercharged Nuclear Ramjet Propulsion System
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Book Synopsis Preliminary Analysis of Supercharged Nuclear Ramjet Propulsion System by :
Download or read book Preliminary Analysis of Supercharged Nuclear Ramjet Propulsion System written by and published by . This book was released on 1957 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: A preliminary analysis has been made to compare the performance.of a ceramic ramjet reactor powerplant, such as described in General Electric Report No. XDC-56-5-81, with that of such a powerplant supercharged by a metallic-vapor-cycle compressor jet. Performance at sea level, Mach 2.5 is ·reported for the vapor-cycle compressor jet alone, for the ramjet alone, and for the compressor jet - ramjet combination. Results indicate that adding the compressor-jet as a supercharger for the ramjet provides an increase in specific thrust of about 20 percent over that of the ramjet alone, with an attendant increase in thermal efficiency of about 20 percent over that of the ramjet alone.
Book Synopsis Preliminary Analysis of a Nuclear-powered Supersonic Airplane Using Ramjet Engines by : Richard J. Weber
Download or read book Preliminary Analysis of a Nuclear-powered Supersonic Airplane Using Ramjet Engines written by Richard J. Weber and published by . This book was released on 1958 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Analysis of Three Cycles for Nuclear Propulsion of Aircraft by : L.V. Humble
Download or read book Preliminary Analysis of Three Cycles for Nuclear Propulsion of Aircraft written by L.V. Humble and published by . This book was released on 1950 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Nuclear Ramjet Propulsion System by : Theodore C. Merkle
Download or read book The Nuclear Ramjet Propulsion System written by Theodore C. Merkle and published by . This book was released on 1961 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Analysis of a High Temperature Nuclear Reactor Core for Space Vehicle Propulsion by : Lester Goldfisher
Download or read book Preliminary Analysis of a High Temperature Nuclear Reactor Core for Space Vehicle Propulsion written by Lester Goldfisher and published by . This book was released on 1959 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Preliminary Model for Spacecraft Propulsion Performance Analysis Based on Nuclear Gain and Sub-system Mass Power Balances by : S. Chakrabarti
Download or read book A Preliminary Model for Spacecraft Propulsion Performance Analysis Based on Nuclear Gain and Sub-system Mass Power Balances written by S. Chakrabarti and published by . This book was released on 1999 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Reduced-order Analysis of Dual Mode Supersonic Combustion Ramjet Propulsion System by : Vijay Gopal
Download or read book Reduced-order Analysis of Dual Mode Supersonic Combustion Ramjet Propulsion System written by Vijay Gopal and published by . This book was released on 2017 with total page 137 pages. Available in PDF, EPUB and Kindle. Book excerpt: High speed propulsion systems typically possess relatively simple geometry but the complexity involved in the flow characteristics makes their analysis a challenging task. The current research work introduces a reduced order analytical model for a steady operation of dual mode SCRamjet (Supersonic Combustion Ramjet) propulsion system at design and off-design conditions. The model hopes to reduce analysis time and complexity to carry out parametric sweep studies for preliminary design of SCRamjet engines. The analytical model splits the analysis of SCRamjet engine into five interactive components namely: inlet, isolator, injector, burner and nozzle. Each component is modelled using physics of gas-dynamics and semi-empirical relations. The flow characterization of each component and their interactions are modelled carefully based on observed physical phenomenon reported in the existing literature. The model is developed on MATLAB platform providing flexibility to design a parametrized SCRamjet geometry and to select its free stream and fueling conditions for the analysis. The analytical model proposed in the current work is validated with various experimental and computational data of individual components and its reliability for predicting the flow characteristics inside a SCRamjet propulsion system is discussed in detail.
Book Synopsis Preliminary Gas Dynamic Analysis of a Nuclear Rocket System with a Wave Super-heater by : Georges Mokbel Saad
Download or read book Preliminary Gas Dynamic Analysis of a Nuclear Rocket System with a Wave Super-heater written by Georges Mokbel Saad and published by . This book was released on 1962 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Analysis of Hydrogen-rich Hypersonic Ramjet Operation by : Roland Breitwieser
Download or read book Preliminary Analysis of Hydrogen-rich Hypersonic Ramjet Operation written by Roland Breitwieser and published by . This book was released on 1958 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Nuclear Ramjet Propulsion System by :
Download or read book The Nuclear Ramjet Propulsion System written by and published by . This book was released on 1959 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: The most practical nuclear ramjet systems consist of a suituble inlet diffusor system followed by a singlepass, straight-through heat exchanger (reactor) which couples into a typical exhaust nozzle. Within this framework, possibilities ars governed by the aerodynamic requirements of flight, the nuclear requirements of the reactor, the chemical problems associated with breathing air, and the mechanical properties of materials at elevated temperatures. The major research and development areas which must be entered in the actual production of such an engine are discussed. (W.D.M.).
Book Synopsis Analysis of an Open Cycle Gas Core Nuclear Propulsion System Using HD Driven Vortices for Fuel Containment by : Raymond John Sedwick
Download or read book Analysis of an Open Cycle Gas Core Nuclear Propulsion System Using HD Driven Vortices for Fuel Containment written by Raymond John Sedwick and published by . This book was released on 1998 with total page 312 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 1992 with total page 1556 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1979 with total page 840 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Power for Flight by : Jeremy R. Kinney
Download or read book The Power for Flight written by Jeremy R. Kinney and published by Government Printing Office. This book was released on 2018-02-15 with total page 318 pages. Available in PDF, EPUB and Kindle. Book excerpt: The NACA and aircraft propulsion, 1915-1958 -- NASA gets to work, 1958-1975 -- The shift toward commercial aviation, 1966-1975 -- The quest for propulsive efficiency, 1976-1989 -- Propulsion control enters the computer era, 1976-1998 -- Transiting to a new century, 1990-2008 -- Toward the future
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 1992 with total page 1400 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Ramjet Engines by : Mikhail Makarovich Bondari͡u︡k
Download or read book Ramjet Engines written by Mikhail Makarovich Bondari͡u︡k and published by . This book was released on 1969 with total page 466 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Fundamentals of Aircraft and Rocket Propulsion by : Ahmed F. El-Sayed
Download or read book Fundamentals of Aircraft and Rocket Propulsion written by Ahmed F. El-Sayed and published by Springer. This book was released on 2016-05-25 with total page 1025 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book provides a comprehensive basics-to-advanced course in an aero-thermal science vital to the design of engines for either type of craft. The text classifies engines powering aircraft and single/multi-stage rockets, and derives performance parameters for both from basic aerodynamics and thermodynamics laws. Each type of engine is analyzed for optimum performance goals, and mission-appropriate engines selection is explained. Fundamentals of Aircraft and Rocket Propulsion provides information about and analyses of: thermodynamic cycles of shaft engines (piston, turboprop, turboshaft and propfan); jet engines (pulsejet, pulse detonation engine, ramjet, scramjet, turbojet and turbofan); chemical and non-chemical rocket engines; conceptual design of modular rocket engines (combustor, nozzle and turbopumps); and conceptual design of different modules of aero-engines in their design and off-design state. Aimed at graduate and final-year undergraduate students, this textbook provides a thorough grounding in the history and classification of both aircraft and rocket engines, important design features of all the engines detailed, and particular consideration of special aircraft such as unmanned aerial and short/vertical takeoff and landing aircraft. End-of-chapter exercises make this a valuable student resource, and the provision of a downloadable solutions manual will be of further benefit for course instructors.
