36th Aiaa Asme Sae Asee Joint Propulsion Conference Exhibit 2000 3100 2000 3149
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36th Aiaa Asme Sae Asee Joint Propulsion Conference Exhibit 2000 3100 2000 3149
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Author :
language : en
Publisher:
Release Date : 2000
36th Aiaa Asme Sae Asee Joint Propulsion Conference Exhibit 2000 3100 2000 3149 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with Airplanes categories.
Measurement Instrumentation And Sensors Handbook Second Edition
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Author : John G. Webster
language : en
Publisher: CRC Press
Release Date : 2014-01-29
Measurement Instrumentation And Sensors Handbook Second Edition written by John G. Webster and has been published by CRC Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2014-01-29 with Medical categories.
The Second Edition of the bestselling Measurement, Instrumentation, and Sensors Handbook brings together all aspects of the design and implementation of measurement, instrumentation, and sensors. Reflecting the current state of the art, it describes the use of instruments and techniques for performing practical measurements in engineering, physics, chemistry, and the life sciences and discusses processing systems, automatic data acquisition, reduction and analysis, operation characteristics, accuracy, errors, calibrations, and the incorporation of standards for control purposes. Organized according to measurement problem, the Spatial, Mechanical, Thermal, and Radiation Measurement volume of the Second Edition: Contains contributions from field experts, new chapters, and updates to all 96 existing chapters Covers instrumentation and measurement concepts, spatial and mechanical variables, displacement, acoustics, flow and spot velocity, radiation, wireless sensors and instrumentation, and control and human factors A concise and useful reference for engineers, scientists, academic faculty, students, designers, managers, and industry professionals involved in instrumentation and measurement research and development, Measurement, Instrumentation, and Sensors Handbook, Second Edition: Spatial, Mechanical, Thermal, and Radiation Measurement provides readers with a greater understanding of advanced applications.
The Use Of Electrostatic Probes To Characterize The Discharge Plasma Structure And Identify Discharge Cathode Erosion Mechanisms In Ring Cusp Ion Thrusters
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Author : Daniel Andrew Herman
language : en
Publisher:
Release Date : 2005
The Use Of Electrostatic Probes To Characterize The Discharge Plasma Structure And Identify Discharge Cathode Erosion Mechanisms In Ring Cusp Ion Thrusters written by Daniel Andrew Herman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2005 with categories.
Inductive Measurement Of Plasma Jet Electrical Conductivity
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Author : M. W. Turner
language : en
Publisher:
Release Date : 2001
Inductive Measurement Of Plasma Jet Electrical Conductivity written by M. W. Turner and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2001 with Electric arc categories.
Measurement of plasma jet electrical conductivity has utility in the development of explosively driven magnetohydrodynamic (MHD) energy converters as well as magnetic flux compression reaction chambers for nuclear/chemical pulse propulsion and power. Within these types of reactors, the physical parameter of critical importance to underlying MHD processes is the magnetic Reynolds number, the value of which depends upon the product of plasma electrical conductivity and velocity. Therefore, a thorough understanding of MHD phenomena at high magnetic Reynolds number is essential, and methods are needed for the accurate and reliable measurement of electrical conductivity in high-speed plasma jets. It is well known that direct measurements using electrodes suffer from large surface resistances, and an electrodeless technique is desired.
Shock Tube Research Proceedings Of The Eighth International Shock Tube Symposium Imperial College London 5 8 July 1971
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Author : J. L. Stollery
language : en
Publisher: Chapman & Hall
Release Date : 1971
Shock Tube Research Proceedings Of The Eighth International Shock Tube Symposium Imperial College London 5 8 July 1971 written by J. L. Stollery and has been published by Chapman & Hall this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Science categories.
Linear Aerospike Sr 71 Experiment Lasre Aerospace Propulsion Hazard Mitigation Systems
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Author : Masashi Mizukami
language : en
Publisher:
Release Date : 1998
Linear Aerospike Sr 71 Experiment Lasre Aerospace Propulsion Hazard Mitigation Systems written by Masashi Mizukami and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Airplanes categories.
Unsteady Combustion
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Author : F. Culick
language : en
Publisher: Springer Science & Business Media
Release Date : 2012-12-06
Unsteady Combustion written by F. Culick and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-12-06 with Technology & Engineering categories.
This book contains selected papers prepared for the NATO Advanced Study Institute on "Unsteady Combustion", which was held in Praia da Granja, Portugal, 6-17 September 1993. Approximately 100 delegates from 14 countries attended. The Institute was the most recent in a series beginning with "Instrumentation for Combustion and Flow in Engines", held in Vimeiro, Portugal 1987 and followed by "Combusting Flow Diagnostics" conducted in Montechoro, Portugal in 1990. Together, these three Institutes have covered a wide range of experimental and theoretical topics arising in the research and development of combustion systems with particular emphasis on gas-turbine combustors and internal combustion engines. The emphasis has evolved roughly from instrumentation and experimental techniques to the mixture of experiment, theory and computational work covered in the present volume. As the title of this book implies, the chief aim of this Institute was to provide a broad sampling of problems arising with time-dependent behaviour in combustors. In fact, of course, that intention encompasses practically all possibilities, for "steady" combustion hardly exists if one looks sufficiently closely at the processes in a combustion chamber. The point really is that, apart from the excellent paper by Bahr (Chapter 10) discussing the technology of combustors for aircraft gas turbines, little attention is directed to matters of steady performance. The volume is divided into three parts devoted to the subjects of combustion-induced oscillations; combustion in internal combustion engines; and experimental techniques and modelling.
Initial Flight Test Evaluation Of The F 15 Active Axisymmetric Vectoring Nozzle Performance
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Author : John S. Orme
language : en
Publisher:
Release Date : 1998
Initial Flight Test Evaluation Of The F 15 Active Axisymmetric Vectoring Nozzle Performance written by John S. Orme and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Black Widow (Night fighter plane) categories.
A full envelope database of a thrust-vectoring axisymmetric nozzle perfomance for the Pratt & Whitney Pitch/Yaw Balance Beam Nozzle (P/YBBN) is being developed using the F-15 Advanced Control Technology for Integrated Vehicles (ACTIVE) aircraft. At this time, flight research has been completed for steady-state pitch vector angles up to 20 deg. at an altitude of 30,000 ft from low power settings to maximum afterburner power. The nozzle performance database includes vector forces, internal nozzle pressures, and temperatures all of which can be used for regression analysis modeling. The database was used to substantiate a set of nozzle performance data from wind tunnel testing and computational fluid dynamic analyses. Findings from initial flight research at Mach 0.9 and 1.2 are presented in this paper. The results show that vector efficiency is strongly influenced by power setting. A significant discrepancy in nozzle performance has been discovered between predicted and measured results during vectoring.
Wave Turbine Analysis Tool Development
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Author : Gerard E. Welch
language : en
Publisher:
Release Date : 1998
Wave Turbine Analysis Tool Development written by Gerard E. Welch and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with categories.
A quasi-one-dimensional (Q-1-D) computational fluid dynamic solver, previously developed and validated for pressure-exchanger wave rotors, is extended in the present work to include the blade forces of power producing wave rotors (i.e., wave turbines). The accuracy of the single-passage Q-1-D solver is assessed relative to two two-dimensional solvers: a single-passage code and a multi-block stator/rotor/stator code. Comparisons of computed results for inviscid, steady and unsteady flows in passage geometries typical of wave rotors reveal that the blade force model is accurate and that the correlation (effective stress and heat flux) terms of the Q-1-D passage-averaged formulation can be neglected. The ends of the rotor passages pose particular challenges to Q-1-D formulations because the flow there must at times deviate significantly from the mean camber line angle to match the port flow fields. This problem is most acute during the opening and closing of the rotor passages. An example sub-model is developed to account for the deviation between the flow departure angle and the mean camber line exit angle that occurs as an inviscid flow decelerates to meet a uniform pressure boundary. Comparisons of results from four-port wave turbine simulations reveal that the Q-1-D solver currently overpredicts wave turbine performance levels and highlight the need to devote future effort to the boundary conditions and sub-models of the Q-1-D solver.
An Incidence Loss Model For Wave Rotors With Axially Aligned Passages
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Author : Daniel E. Paxson
language : en
Publisher:
Release Date : 1998
An Incidence Loss Model For Wave Rotors With Axially Aligned Passages written by Daniel E. Paxson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Aerodynamics categories.