Investigation of Hypersonic Shock-induced Combustion in a Hydrogen-air System

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ISBN 13 :
Total Pages : 110 pages
Book Rating : 4.:/5 (316 download)

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Book Synopsis Investigation of Hypersonic Shock-induced Combustion in a Hydrogen-air System by : J. K. Ahuja

Download or read book Investigation of Hypersonic Shock-induced Combustion in a Hydrogen-air System written by J. K. Ahuja and published by . This book was released on 1992 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Parametric Study of Shock-induced Combustion in a Hydrogen-air System

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis A Parametric Study of Shock-induced Combustion in a Hydrogen-air System by : J. K. Ahuja

Download or read book A Parametric Study of Shock-induced Combustion in a Hydrogen-air System written by J. K. Ahuja and published by . This book was released on 1994 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Preliminary Study of Stationary Shock-induced Combustion with Hydrogen-air Mixtures

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ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis A Preliminary Study of Stationary Shock-induced Combustion with Hydrogen-air Mixtures by : R. P. Rhodes

Download or read book A Preliminary Study of Stationary Shock-induced Combustion with Hydrogen-air Mixtures written by R. P. Rhodes and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: DESCRIPTORS: Rocket motors *Hydrogen, *Air, *Combustion, *Ignition, Gases, Shock waves, Fuel injection, Fuel injectors, Supersonic flow, Schlieren photography, Mixtures, Combustion cham ers, Combustion chamber gas s. A study of the shock-induced combustion of hydrogen-air mixtures was made in a small Mach number 3 wind tunnel at a total pressure level of 45 psia. Combustion was induced by a normal shock wave which resulted from the interaction of two oblique shock wave produced by wedges on the tunnel walls. Significantly different phenomena were observed when the fuel injector was moved from the subsonic portion of the n zzle into the throat. With fuel injection in the throat, ignition denoted by emission glow from the sodium introduced with the hydrogen did not occur until some distance downstream of the normal shock wave. Some data are presented showing this delay as a function of the static temperature behind the shock wave. (A thor).

Investigation of Shock-induced Combustion Past Blunt Projectiles

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ISBN 13 :
Total Pages : 196 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Investigation of Shock-induced Combustion Past Blunt Projectiles by : J. K. Ahuja

Download or read book Investigation of Shock-induced Combustion Past Blunt Projectiles written by J. K. Ahuja and published by . This book was released on 1996 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Theoretical and Experimental Investigation of Supersonic Combustion

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ISBN 13 :
Total Pages : 136 pages
Book Rating : 4.3/5 (126 download)

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Book Synopsis Theoretical and Experimental Investigation of Supersonic Combustion by : Antonio Ferri

Download or read book Theoretical and Experimental Investigation of Supersonic Combustion written by Antonio Ferri and published by . This book was released on 1962 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt: A theoretical and experimental investigation of mixing and supersonic combustion is presented. A review of the problem under investigation is given. Then an analysis of inviscid flow fields with a finite rate chemistry for a hydrogen-air reaction is presented, an an analysis of a turbulent mixing for flows with large density gradients with no chemical reaction is presented. The analysis is compared wit the experimental results. Results of the experiments in upersonic combustion are presented. (Author).

A Fully Implicit Time Accurate Method for Hypersonic Combustion

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Fully Implicit Time Accurate Method for Hypersonic Combustion by : Shaye Yungster

Download or read book A Fully Implicit Time Accurate Method for Hypersonic Combustion written by Shaye Yungster and published by . This book was released on 1994 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Airbreathing Propulsion

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Publisher : AIAA
ISBN 13 : 9781563470356
Total Pages : 632 pages
Book Rating : 4.4/5 (73 download)

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Book Synopsis Hypersonic Airbreathing Propulsion by : William H. Heiser

Download or read book Hypersonic Airbreathing Propulsion written by William H. Heiser and published by AIAA. This book was released on 1994 with total page 632 pages. Available in PDF, EPUB and Kindle. Book excerpt: An almost entirely self-contained engineering textbook primarily for use in undergraduate and graduate courses in airbreathing propulsion. It provides a broad and basic introduction to the elements needed to work in the field as it develops and grows. Homework problems are provided for almost every individual subject. An extensive array of PC-based user-friendly computer programs is provided in order to facilitate repetitious and/or complex calculations. Annotation copyright by Book News, Inc., Portland, OR

Numerical Study of Shock-wave/boundary Layer Interactions in Premixed Hydrogen-air Hypersonic Flows

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Numerical Study of Shock-wave/boundary Layer Interactions in Premixed Hydrogen-air Hypersonic Flows by : Shaye Yungster

Download or read book Numerical Study of Shock-wave/boundary Layer Interactions in Premixed Hydrogen-air Hypersonic Flows written by Shaye Yungster and published by . This book was released on 1991 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Computational Study of Unsteady Shock Induced Combustion of Hydrogen-air Mixtures

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ISBN 13 :
Total Pages : 23 pages
Book Rating : 4.:/5 (976 download)

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Book Synopsis A Computational Study of Unsteady Shock Induced Combustion of Hydrogen-air Mixtures by : Myles A. Sussman

Download or read book A Computational Study of Unsteady Shock Induced Combustion of Hydrogen-air Mixtures written by Myles A. Sussman and published by . This book was released on 1994 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 702 pages
Book Rating : 4.:/5 (31 download)

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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 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Numerical Simulation of Shock-induced Combustion in a Superdetonative Hydrogen-air System

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ISBN 13 :
Total Pages : 13 pages
Book Rating : 4.:/5 (977 download)

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Book Synopsis Numerical Simulation of Shock-induced Combustion in a Superdetonative Hydrogen-air System by : J. K. Ahuja

Download or read book Numerical Simulation of Shock-induced Combustion in a Superdetonative Hydrogen-air System written by J. K. Ahuja and published by . This book was released on 1993 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Turbulent Reactive Flows

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Publisher : Springer Science & Business Media
ISBN 13 : 146139631X
Total Pages : 958 pages
Book Rating : 4.4/5 (613 download)

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Book Synopsis Turbulent Reactive Flows by : R. Borghi

Download or read book Turbulent Reactive Flows written by R. Borghi and published by Springer Science & Business Media. This book was released on 2013-03-08 with total page 958 pages. Available in PDF, EPUB and Kindle. Book excerpt: Turbulent reactive flows are of common occurrance in combustion engineering, chemical reactor technology and various types of engines producing power and thrust utilizing chemical and nuclear fuels. Pollutant formation and dispersion in the atmospheric environment and in rivers, lakes and ocean also involve interactions between turbulence, chemical reactivity and heat and mass transfer processes. Considerable advances have occurred over the past twenty years in the understanding, analysis, measurement, prediction and control of turbulent reactive flows. Two main contributors to such advances are improvements in instrumentation and spectacular growth in computation: hardware, sciences and skills and data processing software, each leading to developments in others. Turbulence presents several features that are situation-specific. Both for that reason and a number of others, it is yet difficult to visualize a so-called solution of the turbulence problem or even a generalized approach to the problem. It appears that recognition of patterns and structures in turbulent flow and their study based on considerations of stability, interactions, chaos and fractal character may be opening up an avenue of research that may be leading to a generalized approach to classification and analysis and, possibly, prediction of specific processes in the flowfield. Predictions for engineering use, on the other hand, can be foreseen for sometime to come to depend upon modeling of selected features of turbulence at various levels of sophistication dictated by perceived need and available capability.

Inviscid On-design Propulsive Characteristics of Hypersonic Shock-induced Combustion Ramjets

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Publisher : North York, Ont. : Institute for Aerospace Studies, University of Toronto
ISBN 13 :
Total Pages : 348 pages
Book Rating : 4.:/5 (972 download)

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Book Synopsis Inviscid On-design Propulsive Characteristics of Hypersonic Shock-induced Combustion Ramjets by : Jean Pascal Sislian

Download or read book Inviscid On-design Propulsive Characteristics of Hypersonic Shock-induced Combustion Ramjets written by Jean Pascal Sislian and published by North York, Ont. : Institute for Aerospace Studies, University of Toronto. This book was released on 1997 with total page 348 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Incomplete Fuel/air Mixing on the Performance Characteristics of Hypersonic Shock-induced Combustion Ramjets (shcramjets)

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ISBN 13 :
Total Pages : 145 pages
Book Rating : 4.:/5 (976 download)

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Book Synopsis Effects of Incomplete Fuel/air Mixing on the Performance Characteristics of Hypersonic Shock-induced Combustion Ramjets (shcramjets) by : Jurgen Schumacher

Download or read book Effects of Incomplete Fuel/air Mixing on the Performance Characteristics of Hypersonic Shock-induced Combustion Ramjets (shcramjets) written by Jurgen Schumacher and published by . This book was released on 1995 with total page 145 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Inviscid Off-design Propulsive Performance of Hypersonic Shock-induced Combustion Ramjets

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Publisher : North York, Ont. : Institute for Aerospace Studies, University of Toronto
ISBN 13 :
Total Pages : 224 pages
Book Rating : 4.:/5 (379 download)

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Book Synopsis Inviscid Off-design Propulsive Performance of Hypersonic Shock-induced Combustion Ramjets by : Jean Pascal Sislian

Download or read book Inviscid Off-design Propulsive Performance of Hypersonic Shock-induced Combustion Ramjets written by Jean Pascal Sislian and published by North York, Ont. : Institute for Aerospace Studies, University of Toronto. This book was released on 1997 with total page 224 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigations Into Shock-Induced Enhancement of Mixing and Combustion in Supersonic Burners

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ISBN 13 :
Total Pages : 23 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Investigations Into Shock-Induced Enhancement of Mixing and Combustion in Supersonic Burners by : Frank E. Marble

Download or read book Investigations Into Shock-Induced Enhancement of Mixing and Combustion in Supersonic Burners written by Frank E. Marble and published by . This book was released on 1987 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt: Modifications to three major facilities at Caltech, carried out in preparation for an extensive investigation of shock enhanced mixing and combustion in supersonic combustion ramjets, has progressed according to schedule. Work is complete on the GALCIT 17-inch shock tube and on the Unsteady Combustion Facility, and they are operating as planned. Extensive improvement of the optical diagnostics and data acquisition equipment for both of these is nearly complete. Design of the new heated-hydrogen leg for the Hydrogen/Fluorine facility has been simplified considerably from the original concept and is progressing satisfactorily. Extensive computational studies of the interaction between weak shock waves and isolated regions of hydrogen embedded in air has revealed a behavior which suggests that considerable technological advantage may accrue by the use of multiple weak shocks to enhance mixing. Keywords: Supersonic combustion; Vortex burning mixing; Shear layers vorticity generation; Shock enhanced mixing.

On the Use of Shock-induced Combustion in Hypersonic Engines

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis On the Use of Shock-induced Combustion in Hypersonic Engines by : Wallace Chinitz

Download or read book On the Use of Shock-induced Combustion in Hypersonic Engines written by Wallace Chinitz and published by . This book was released on 1996 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: