Use of Fluidic Oscillator to Measure Fuel-air Ratios of Combustion Gases PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Use of Fluidic Oscillator to Measure Fuel-air Ratios of Combustion Gases PDF full book. Access full book title Use of Fluidic Oscillator to Measure Fuel-air Ratios of Combustion Gases by Stephen M. Riddlebaugh. Download full books in PDF and EPUB format.
Author: Stephen M. Riddlebaugh
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 28
Get Book Here
Book Description
Author: Stephen M. Riddlebaugh
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 28
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 594
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 272
Get Book Here
Book Description
Author: W. Cornelius
Publisher: Springer Science & Business Media
ISBN: 1468419986
Category : Science
Languages : en
Pages : 474
Get Book Here
Book Description
This volume documents the proceedings of the Symposium on Emissions from Continuous Combustion Systems that was held at the General Motors Research Laboratories, Warren, Michigan on September 27 and 28, 1971. This symposium was the fifteenth in an annual series presented by the Research Laboratories. Each symposium has covered a different technical discipline. To be selected as the theme of a symposium, the subject must be timely and of vital interest to General Motors as well as to the technical community at large. For each symposium, the practice is to solicit papers at the forefront of research from recognized authorities in the technical discipline of interest. Approximately sixty scientists and engineers from academic, government and industrial circles in this country and abroad are then invited to join about an equal number of General Motors technical personnel to discuss freely the commissioned papers. The technical portion of the meeting is supplemented by social functions at which ample time is afforded for informal exchanges of ideas amongst the participants. By such a direct interaction of a small and select group of informed participants, it is hoped to extend the boundaries of research in the selected technical field.
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1388
Get Book Here
Book Description
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1408
Get Book Here
Book Description
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1446
Get Book Here
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index
Author:
Publisher:
ISBN:
Category : Air
Languages : en
Pages : 666
Get Book Here
Book Description
Author: United States. Environmental Protection Agency
Publisher:
ISBN:
Category : Air
Languages : en
Pages : 646
Get Book Here
Book Description
Author: D. E. Chriss
Publisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 52
Get Book Here
Book Description
An experimental investigation of ducted, two stream, subsonic, reactive, turbulent jet mixing with recirculation was conducted. A primary jet of air at a mass flow rate of 0.075 lb/sec and velocity of 700 ft/sec was surrounded by an outer, low velocity, hydrogen stream. Data were obtained with hydrogen-air ratios of 0.143 and 0.107. The duct-to-inner nozzle diameter ratio was ten. Radial distributions of hydrogen mass fraction, mean axial velocity, turbulence intensity, and total pressure as well as axial distributions of wall hydrogen mass fraction and wall static pressure are presented for axial stations from one-half to five duct diameters from the nozzle exit plane. Comparison of the experimental data with calculations assuming frozen or equilibrium chemistry indicate that he measured velocity, pressure, and composition data are, in general, self-consistent. The maximum turbulent intensities which occurred in the center of the mixing layer and within the recirculation eddy were very high having values of 20 percent of the jet exit velocity. The velocity and composition field indicate that, while and mixing in the reactive flow field is slower than for the nonreactive case, the reaction had little effect on the size and location of the recirculation zone within the mixing duct.
