Author: G. Balu
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Experimental Investigation of Isolator for Supersonic Combustion
Experimental Investigation of Inlet-combustor Isolators for a Dual-mode Scramjet at a Mach Number of 4
Author: Saied Emami
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 96
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 96
Book Description
Experimental Investigation of Inlet-Combustor Isolators for a Dual-Mode Scramjet at a Mach Number of 4
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722387747
Category :
Languages : en
Pages : 96
Book Description
This report details experimentally derived operational characteristics of numerous two-dimensional planar inlet-combustor isolator configurations at a Mach number of 4. Variations in geometry included (1) inlet cowl length; (2) inlet cowl rotation angle; (3) isolator length; and (4) utilization of a rearward-facing isolator step. To obtain inlet-isolator maximum pressure-rise data relevant to ramjet-engine combustion operation, configurations were mechanically back pressured. Results demonstrated that the combined inlet-isolator maximum back-pressure capability increases as a function of isolator length and contraction ratio, and that the initiation of unstart is nearly independent of inlet cowl length, inlet cowl contraction ratio, and mass capture. Additionally, data are presented quantifying the initiation of inlet unstarts and the corresponding unstart pressure levels. Emami, Saied and Trexler, Carl A. and Auslender, Aaron H. and Weidner, John P. Langley Research Center...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722387747
Category :
Languages : en
Pages : 96
Book Description
This report details experimentally derived operational characteristics of numerous two-dimensional planar inlet-combustor isolator configurations at a Mach number of 4. Variations in geometry included (1) inlet cowl length; (2) inlet cowl rotation angle; (3) isolator length; and (4) utilization of a rearward-facing isolator step. To obtain inlet-isolator maximum pressure-rise data relevant to ramjet-engine combustion operation, configurations were mechanically back pressured. Results demonstrated that the combined inlet-isolator maximum back-pressure capability increases as a function of isolator length and contraction ratio, and that the initiation of unstart is nearly independent of inlet cowl length, inlet cowl contraction ratio, and mass capture. Additionally, data are presented quantifying the initiation of inlet unstarts and the corresponding unstart pressure levels. Emami, Saied and Trexler, Carl A. and Auslender, Aaron H. and Weidner, John P. Langley Research Center...
Numerical and Experimental Studies on Combustion Engines and Vehicles
Author: Paweł Woś
Publisher: BoD – Books on Demand
ISBN: 1839680326
Category : Technology & Engineering
Languages : en
Pages : 176
Book Description
The matters discussed and presented in the chapters of this book cover a wide spectrum of topics and research methods commonly used in the field of engine combustion technology and vehicle functional systems. This book contains the results of both computational analyses and experimental studies on jet and reciprocating combustion engines as well heavy-duty onroad vehicles. Special attention is devoted to research and measures toward preventing the emission of harmful exhaust components, reducing fuel consumption or using unconventional methods of engine fueling or using renewable and alternative fuels in different applications. Some technical improvements in design and control of vehicle systems are also presented.
Publisher: BoD – Books on Demand
ISBN: 1839680326
Category : Technology & Engineering
Languages : en
Pages : 176
Book Description
The matters discussed and presented in the chapters of this book cover a wide spectrum of topics and research methods commonly used in the field of engine combustion technology and vehicle functional systems. This book contains the results of both computational analyses and experimental studies on jet and reciprocating combustion engines as well heavy-duty onroad vehicles. Special attention is devoted to research and measures toward preventing the emission of harmful exhaust components, reducing fuel consumption or using unconventional methods of engine fueling or using renewable and alternative fuels in different applications. Some technical improvements in design and control of vehicle systems are also presented.
A Numerical Investigation of the Influence of Cross-section Geometry on Scramjet Isolator Performance
Author: Ryan Steven Glasby
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 178
Book Description
Abstract: A numerical investigation of the flow in scramjet isolators has been conducted in an effort to determine the influence of cross-section geometry on isolator performance. Flow in axi-symmetric isolator configurations is compared with isolators having rectangular cross-section geometries. In this study, various combinations of inflow Mach number, cross-section area, and back pressure are specified as input data in the computational procedure to evaluate performance characteristics of the given isolators. The length and location of the shock train are generally regarded among key flow phenomena that influence isolator performance. This study shows that, for a range of incoming Mach numbers and different cross-section geometries, an isolator with an axi-symmetric cross- section performs better than one with a rectangular cross-section. This can be attributed largely to losses associated with corner flow in isolators having a rectangular crosssection. In general, the results of this study indicate that improvements in isolator performance are attained in isolators having axi-symmetric cross-sections and that improvements increase with increasing Mach number. The numerical results are compared with experimental data, and the agreement with the trends of the experimental data is most encouraging.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 178
Book Description
Abstract: A numerical investigation of the flow in scramjet isolators has been conducted in an effort to determine the influence of cross-section geometry on isolator performance. Flow in axi-symmetric isolator configurations is compared with isolators having rectangular cross-section geometries. In this study, various combinations of inflow Mach number, cross-section area, and back pressure are specified as input data in the computational procedure to evaluate performance characteristics of the given isolators. The length and location of the shock train are generally regarded among key flow phenomena that influence isolator performance. This study shows that, for a range of incoming Mach numbers and different cross-section geometries, an isolator with an axi-symmetric cross- section performs better than one with a rectangular cross-section. This can be attributed largely to losses associated with corner flow in isolators having a rectangular crosssection. In general, the results of this study indicate that improvements in isolator performance are attained in isolators having axi-symmetric cross-sections and that improvements increase with increasing Mach number. The numerical results are compared with experimental data, and the agreement with the trends of the experimental data is most encouraging.
Experimental Investigation of a Supersonic Combustion Flowfield Employing Staged Transverse Injection Behind a Rearward-facing Step
Author: John D. Abbitt
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 02-4100 - 02-4149
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 624
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 624
Book Description
Experimental Investigation of Supersonic Combustion of Liquid Hydrocarbon Fuel Using Barbotage in the Aeroramp Configuration at M
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This report results from a contract tasking TsAGl as follows: The contractor will investigate combustion of kerosene using barbotage by hydrogen and air in the aeroramp configuration at M=2.5 as described in his proposal dated 1 Jun 98.
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This report results from a contract tasking TsAGl as follows: The contractor will investigate combustion of kerosene using barbotage by hydrogen and air in the aeroramp configuration at M=2.5 as described in his proposal dated 1 Jun 98.
Advances in Mechanical and Materials Technology
Author: Kannan Govindan
Publisher: Springer Nature
ISBN: 9811627940
Category : Technology & Engineering
Languages : en
Pages : 1422
Book Description
This book presents select papers from the International Conference on Energy, Material Sciences and Mechanical Engineering (EMSME) - 2020. The book covers the three core areas of energy, material sciences and mechanical engineering. The topics covered include non-conventional energy resources, energy harvesting, polymers, composites, 2D materials, systems engineering, materials engineering, micro-machining, renewable energy, industrial engineering and additive manufacturing. This book will be useful to researchers and professionals working in the areas of mechanical and industrial engineering, materials applications, and energy technology.
Publisher: Springer Nature
ISBN: 9811627940
Category : Technology & Engineering
Languages : en
Pages : 1422
Book Description
This book presents select papers from the International Conference on Energy, Material Sciences and Mechanical Engineering (EMSME) - 2020. The book covers the three core areas of energy, material sciences and mechanical engineering. The topics covered include non-conventional energy resources, energy harvesting, polymers, composites, 2D materials, systems engineering, materials engineering, micro-machining, renewable energy, industrial engineering and additive manufacturing. This book will be useful to researchers and professionals working in the areas of mechanical and industrial engineering, materials applications, and energy technology.
Experimental Studies on H2/air Supersonic Combustion
Author: Yu Gong
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description