Scramjets

Scramjets
Author: Mostafa Barzegar Gerdroodbary
Publsiher: Butterworth-Heinemann
Total Pages: 228
Release: 2020-07-21
ISBN 10: 0128211407
ISBN 13: 9780128211403
Language: EN, FR, DE, ES & NL

Scramjets Book Review:

Scramjet engines are a type of jet engine and rely on the combustion of fuel and an oxidizer to produce thrust. While scramjets are conceptually simple, actual implementation is limited by extreme technical challenges. Hypersonic flight within the atmosphere generates immense drag, and temperatures found on the aircraft and within the engine can be much greater than that of the surrounding air. Maintaining combustion in the supersonic flow presents additional challenges, as the fuel must be injected, mixed, ignited, and burned within milliseconds. Fuel mixing, along with the configuration and positioning of the injectors and the boundary conditions, play a key role in combustion efficiency. Scramjets: Fuel Mixing and Injection Systems discusses how fuel mixing efficiency and the advantage of injection systems can enhance the performance of the scramjets. The book begins with the introduction of the supersonic combustion chamber and explains the main parameters on the mixing rate. The configuration of scramjets is then introduced with special emphasis on the main effective parameters on the mixing of fuel inside the scramjets. In addition, basic concepts and principles on the mixing rate and fuel distribution within scramjets are presented. Main effective parameters such as range of fuel concentration for the efficient combustion, pressure of fuel jet and various arrangement of jet injections are also explained. This book is for aeronautical and mechanical engineers as well as those working in supersonic combustion who need to know the effects of compressibility on combustion, of shocks on mixing and on chemical reactions, and vorticity on the flame anchoring. Explains the main applicable approaches for enhancement of supersonic combustion engines and the new techniques of fuel injection Shows how the interaction of main air stream with fuel injections can develop the mixing inside the scramjets Presents results of numerical simulations and how they can be used for the development of the combustion engines

Really High Speed Propulsion by Scramjets

Really High Speed Propulsion by Scramjets
Author: E. T. CURRAN
Publsiher: Unknown
Total Pages: 35
Release: 1965
ISBN 10: 1928374650XXX
ISBN 13: WISC:89078553070
Language: EN, FR, DE, ES & NL

Really High Speed Propulsion by Scramjets Book Review:

The high overall efficiency of the scramjet engine is potentially maintained over the speed range from Mach 5 to 20. At higher speeds, hydrogen fuel is essential and a fixed geometry appears feasible. Optimization of the intake diffusion can be carried out most easily in terms of the intake process efficiency and velocity ratio. The optimum amount of diffusion is reduced when realistic nozzle losses are included. The development of a hypersonic flight test vehicle is recommended.

A forebody design technique for highly integrated botton mounted scramjets with application to a hypersonic research airplane

A forebody design technique for highly integrated botton mounted scramjets with application to a hypersonic research airplane
Author: C. L. W. Edwards
Publsiher: Unknown
Total Pages: 29
Release: 1976
ISBN 10: 1928374650XXX
ISBN 13: UIUC:30112106911511
Language: EN, FR, DE, ES & NL

A forebody design technique for highly integrated botton mounted scramjets with application to a hypersonic research airplane Book Review:

The Official Guide for GMAT Review

The Official Guide for GMAT Review
Author: GMAC (Graduate Management Admission Council)
Publsiher: John Wiley & Sons
Total Pages: 840
Release: 2012-04-13
ISBN 10: 1118237382
ISBN 13: 9781118237380
Language: EN, FR, DE, ES & NL

The Official Guide for GMAT Review Book Review:

Scramjet Combustion

Scramjet Combustion
Author: Gautam Choubey,Manvendra Tiwari
Publsiher: Butterworth-Heinemann
Total Pages: 196
Release: 2022-07-20
ISBN 10: 0323995667
ISBN 13: 9780323995665
Language: EN, FR, DE, ES & NL

Scramjet Combustion Book Review:

Scramjet Combustion explores the development of a high-speed scramjet engine operating in the supersonic/hypersonic range for various air and space transport applications. The book explains the basic structure, components, working cycle, and the relevant governing equations in a clear manner that speaks to both advanced and more novice audiences. Particular attention is paid to efficient air–fuel combustion, looking at both the underlying fundamentals of combustion as well strategies for obtaining optimum combustion efficiency. Methods for reaching the chemically correct air–fuel ratio, subsequent flame, and combustion stabilization as air enters at supersonic speed are also outlined. Further, it includes the continuous on-going efforts, innovations, and advances with respect to the design modification of scramjet combustors, as well as different strategies of fuel injections for obtaining augmented performance while highlighting the current and future challenges. Outlines the fundamentals of scramjet engines including their basic structure and components, working cycle, governing equations, and combustion fundamentals affecting the combustion and mixing processes Presents new design modifications of scramjet combustors and different fuel injection strategies including combined fuel injection approaches Discusses core topics such as chemical kinetics in supersonic flow, fuel–air mixing methods, strategies for combating combustion difficulties, and subsequent flame and combustion stabilization that can be applied to scramjets Describes the pedagogy for computational approaches in simulating supersonic flows

Scramjet Propulsion

Scramjet Propulsion
Author: E. T. Curran,S. N. B. Murthy
Publsiher: AIAA
Total Pages: 1293
Release: 2001
ISBN 10: 9781600864414
ISBN 13: 1600864414
Language: EN, FR, DE, ES & NL

Scramjet Propulsion Book Review:

The Hypersonic Revolution From Scramjet to the national aero space plane 1964 1986

The Hypersonic Revolution  From Scramjet to the national aero space plane  1964 1986
Author: Anonim
Publsiher: Unknown
Total Pages: 135
Release: 1998
ISBN 10: 1928374650XXX
ISBN 13: PURD:32754068873292
Language: EN, FR, DE, ES & NL

The Hypersonic Revolution From Scramjet to the national aero space plane 1964 1986 Book Review:

The Official Guide for GMAT Review 2015 with Online Question Bank and Exclusive Video

The Official Guide for GMAT Review 2015 with Online Question Bank and Exclusive Video
Author: Graduate Management Admission Council (GMAC)
Publsiher: John Wiley & Sons
Total Pages: 840
Release: 2014-07-08
ISBN 10: 1118914090
ISBN 13: 9781118914090
Language: EN, FR, DE, ES & NL

The Official Guide for GMAT Review 2015 with Online Question Bank and Exclusive Video Book Review:

This is the only official study guide from the creators of the test and delivers more than 900 retired GMAT® questions and answer explanations and a 100- question diagnostic exam to help focus your test preparation efforts. NEW to The Official Guide for GMAT® Review 2015: Access to the online Question Bank including more than 900 practice questions of all types with answers and explanations, math review, essay topics, and a diagnostic test, as well as access to 50 online integrated reasoning questions. Exclusive access to videos from real test takers and GMAC staff who share insight and tips on GMAT® preparation.

Applied and Computational Fluid Mechanics

Applied and Computational Fluid Mechanics
Author: Scott Post
Publsiher: Jones & Bartlett Publishers
Total Pages: 524
Release: 2010-01-30
ISBN 10: 144965584X
ISBN 13: 9781449655846
Language: EN, FR, DE, ES & NL

Applied and Computational Fluid Mechanics Book Review:

Designed for the fluid mechanics course for mechanical, civil, and aerospace engineering students, or as a reference for professional engineers, this up to date text uses computer algorithms and applications to solve modern problems related to fluid flow, aerodynamics, and thermodynamics. Algorithms and codes for numerical solutions of fluid problems, which can be implemented in programming environments such as MATLAB, are used throughout the book. The author also uses non-language specific algorithms to force the students to think through the logic of the solution technique as they translate the algorithm into the software they are using. The text also includes an introduction to Computational Fluid Dynamics, a well-established method in the design of fluid machinery and heat transfer applications. A DVD accompanies every new printed copy of the book and contains the source code, MATLAB files, third-party simulations, color figures, and more.

The Scramjet Engine

The Scramjet Engine
Author: Corin Segal
Publsiher: Cambridge University Press
Total Pages: 253
Release: 2009-06-22
ISBN 10: 0521838150
ISBN 13: 9780521838153
Language: EN, FR, DE, ES & NL

The Scramjet Engine Book Review:

Demand for high-speed propulsion has renewed development of the supersonic combustion ramjet engine (Scramjet engine) for hypersonic flight applications.

Interrelation Between Scramjet Engine Design Engine Cooling Requirement and Vehicle engine Size Requirement for a Shuttle boost Mission

Interrelation Between Scramjet Engine Design  Engine Cooling Requirement and Vehicle engine Size Requirement for a Shuttle boost Mission
Author: Anonim
Publsiher: Unknown
Total Pages: 405
Release: 1973
ISBN 10: 1928374650XXX
ISBN 13: NASA:31769000493927
Language: EN, FR, DE, ES & NL

Interrelation Between Scramjet Engine Design Engine Cooling Requirement and Vehicle engine Size Requirement for a Shuttle boost Mission Book Review:

The Official Guide for GMAT Review Korean Edition

The Official Guide for GMAT Review  Korean Edition
Author: GMAC (Graduate Management Admission Council)
Publsiher: John Wiley & Sons
Total Pages: 840
Release: 2012-04-26
ISBN 10: 1118429389
ISBN 13: 9781118429389
Language: EN, FR, DE, ES & NL

The Official Guide for GMAT Review Korean Edition Book Review:

Trust the worldwide bestselling study guide to help you prepare for the GMAT! The Official Guide for GMAT Review - 12th Edition Here's what you'll find inside the only book on the market written by the creators of the exam.-More than 800 questions from past GMAT tests - including 250 that have never before been published -Full answers and detailed explanations for all questions -Grammar review covering concepts tested on the GMAT Verbal section -Comprehensive math review of the topics tested on the GMAT Quantitative section -Actual essay topics, sample responses, and scoring information -Questions organized in order of difficulty to save study time Also available: -The Official Guide to GMAT Quantitative Review, 2nd Edition -The Official Guide to GMAT Verbal Review, 2nd Edition.

Facing the Heat Barrier

Facing the Heat Barrier
Author: T.A. Heppenheimer
Publsiher: Courier Dover Publications
Total Pages: 352
Release: 2018-09-12
ISBN 10: 0486834514
ISBN 13: 9780486834511
Language: EN, FR, DE, ES & NL

Facing the Heat Barrier Book Review:

This volume from The NASA History Series presents an overview of the science of hypersonics, the study of flight at speeds at which the physics of flows is dominated by aerodynamic heating. The survey begins during the years immediately following World War II, with the first steps in hypersonic research: the development of missile nose cones and the X-15; the earliest concepts of hypersonic propulsion; and the origin of the scramjet engine. Next, it addresses the re-entry problem, which came to the forefront during the mid-1950s, showing how work in this area supported the manned space program and contributed to the development of the orbital shuttle. Subsequent chapters explore the fading of scramjet studies and the rise of the National Aerospace Plane (NASP) program of 1985–95, which sought to lay groundwork for single-stage vehicles. The program's ultimate shortcomings — in terms of aerodynamics, propulsion, and materials — are discussed, and the book concludes with a look at hypersonics in the post-NASP era, including the development of the X-33 and X-34 launch vehicles, further uses for scramjets, and advances in fluid mechanics. Clearly, ongoing research in hypersonics has yet to reach its full potential, and readers with an interest in aeronautics and astronautics will find this book a fascinating exploration of the field's history and future.

Shock Tunnel Studies of Scramjet Phenomena 1995

Shock Tunnel Studies of Scramjet Phenomena 1995
Author: R. G. Morgan
Publsiher: Unknown
Total Pages: 106
Release: 1997
ISBN 10: 1928374650XXX
ISBN 13: NASA:31769000704786
Language: EN, FR, DE, ES & NL

Shock Tunnel Studies of Scramjet Phenomena 1995 Book Review:

29th International Symposium on Shock Waves 2

29th International Symposium on Shock Waves 2
Author: Riccardo Bonazza,Devesh Ranjan
Publsiher: Springer
Total Pages: 814
Release: 2015-07-10
ISBN 10: 331916838X
ISBN 13: 9783319168388
Language: EN, FR, DE, ES & NL

29th International Symposium on Shock Waves 2 Book Review:

This proceedings present the results of the 29th International Symposium on Shock Waves (ISSW29) which was held in Madison, Wisconsin, U.S.A., from July 14 to July 19, 2013. It was organized by the Wisconsin Shock Tube Laboratory, which is part of the College of Engineering of the University of Wisconsin-Madison. The ISSW29 focused on the following areas: Blast Waves, Chemically Reactive Flows, Detonation and Combustion, Facilities, Flow Visualization, Hypersonic Flow, Ignition, Impact and Compaction, Industrial Applications, Magnetohydrodynamics, Medical and Biological Applications, Nozzle Flow, Numerical Methods, Plasmas, Propulsion, Richtmyer-Meshkov Instability, Shock-Boundary Layer Interaction, Shock Propagation and Reflection, Shock Vortex Interaction, Shock Waves in Condensed Matter, Shock Waves in Multiphase Flow, as well as Shock Waves in Rarefield Flow. The two Volumes contain the papers presented at the symposium and serve as a reference for the participants of the ISSW 29 and individuals interested in these fields.

Fundamentals of Aircraft and Rocket Propulsion

Fundamentals of Aircraft and Rocket Propulsion
Author: Ahmed F. El-Sayed
Publsiher: Springer
Total Pages: 1010
Release: 2016-05-25
ISBN 10: 1447167961
ISBN 13: 9781447167969
Language: EN, FR, DE, ES & NL

Fundamentals of Aircraft and Rocket Propulsion Book Review:

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.

Pitot Survey of Exhaust Flow Field of a 2 D Scramjet Nozzle at Mach 6 with Air Or Freon and Argon Used for Exhaust Simulation

Pitot Survey of Exhaust Flow Field of a 2 D Scramjet Nozzle at Mach 6 with Air Or Freon and Argon Used for Exhaust Simulation
Author: William J. Monta
Publsiher: Unknown
Total Pages: 31
Release: 1992
ISBN 10: 1928374650XXX
ISBN 13: NASA:31769000521404
Language: EN, FR, DE, ES & NL

Pitot Survey of Exhaust Flow Field of a 2 D Scramjet Nozzle at Mach 6 with Air Or Freon and Argon Used for Exhaust Simulation Book Review:

Computational Parametric Study of Sidewall compression Scramjet Inlet Performance at Mach 10

Computational Parametric Study of Sidewall compression Scramjet Inlet Performance at Mach 10
Author: Scott D. Holland
Publsiher: Unknown
Total Pages: 14
Release: 1993
ISBN 10: 1928374650XXX
ISBN 13: NASA:31769000521859
Language: EN, FR, DE, ES & NL

Computational Parametric Study of Sidewall compression Scramjet Inlet Performance at Mach 10 Book Review:

Experimental Investigation of Generic Three dimensional Sidewall compression Scramjet Inlets at Mach 6 in Tetrafluoromethane

Experimental Investigation of Generic Three dimensional Sidewall compression Scramjet Inlets at Mach 6 in Tetrafluoromethane
Author: Scott D. Holland
Publsiher: Unknown
Total Pages: 45
Release: 1993
ISBN 10: 1928374650XXX
ISBN 13: NASA:31769000522519
Language: EN, FR, DE, ES & NL

Experimental Investigation of Generic Three dimensional Sidewall compression Scramjet Inlets at Mach 6 in Tetrafluoromethane Book Review:

Conceptual Study of Rocket scramjet Hybrid Engines in a Lifting Reusable Second Stage

Conceptual Study of Rocket scramjet Hybrid Engines in a Lifting Reusable Second Stage
Author: Andrzej Dobrowolski
Publsiher: Unknown
Total Pages: 52
Release: 1969
ISBN 10: 1928374650XXX
ISBN 13: UIUC:30112106875575
Language: EN, FR, DE, ES & NL

Conceptual Study of Rocket scramjet Hybrid Engines in a Lifting Reusable Second Stage Book Review: