A Numerical Investigation Of Sonic Jet Injection For Aerodynamic Control In Supersonic Turbulent Flow 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 A Numerical Investigation Of Sonic Jet Injection For Aerodynamic Control In Supersonic Turbulent Flow PDF full book. Access full book title A Numerical Investigation Of Sonic Jet Injection For Aerodynamic Control In Supersonic Turbulent Flow.
Author | : Steven W. Clark |
Publisher | : |
Total Pages | : 106 |
Release | : 1992 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download A Numerical Investigation of Sonic Jet Injection for Aerodynamic Control in Supersonic Turbulent Flow Book in PDF, ePub and Kindle
Author | : Steven W. Clark |
Publisher | : |
Total Pages | : |
Release | : 1992 |
Genre | : |
ISBN | : |
Download Numerical Investigation of a Transverse Jet for Supersonic Aerodynamic Control Book in PDF, ePub and Kindle
Author | : Mingbo Sun |
Publisher | : Springer |
Total Pages | : 284 |
Release | : 2019-02-18 |
Genre | : Technology & Engineering |
ISBN | : 9811360251 |
Download Jet in Supersonic Crossflow Book in PDF, ePub and Kindle
Based on research into jets in supersonic crossflow carried out by the authors’ team over the past 15 years, this book summarizes and presents many cutting-edge findings and analyses on this subject. It tackles the complicated mixing process of gas jets and atomization process of liquid jets in supersonic crossflow, and studies their physical mechanisms. Advanced experimental and numerical techniques are applied to further readers’ understanding of atomization, mixing, and combustion of fuel jets in supersonic crossflow, which can promote superior fuel injection design in scramjet engines. The book offers a valuable reference guide for all researchers and engineers working on the design of scramjet engines, and will also benefit graduate students majoring in aeronautical and aerospace engineering.
Author | : Martin Hersch |
Publisher | : |
Total Pages | : 20 |
Release | : 1970 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Optical Study of Sonic and Supersonic Jet Penetration from a Flat Plate Into a Mach 2 Airstream Book in PDF, ePub and Kindle
Author | : William F. Hinson |
Publisher | : |
Total Pages | : 50 |
Release | : 1970 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Experimental Investigation of Multiple-jet Liquid Injection Into Hypersonic Flow Book in PDF, ePub and Kindle
Author | : W. C. Armstrong |
Publisher | : |
Total Pages | : 98 |
Release | : 1976 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Analysis of Three-dimensional Inviscid Supersonic Flow Between a Body and an Outer Wall Book in PDF, ePub and Kindle
The three-dimensional inviscid supersonic flow equations are solved for the flow over a body located within a duct. Numerical solutions are obtained by use of the reference plane method of characteristics technique. Results of the analysis are compared with experimental test body pressure distributions obtained with an off-design jet stretcher system. The analysis is sufficiently general so that a variety of internal flows may be predicted. A computer program listing and an example problem are presented.
Author | : Leo Patrick O'Hare |
Publisher | : |
Total Pages | : 206 |
Release | : 1986 |
Genre | : |
ISBN | : |
Download Numerical Investigation of the Supersonic Flow Through a SCRAMjet Including Hydrogen Injection and Combustion Book in PDF, ePub and Kindle
Author | : Johns Hopkins University. Applied Physics Laboratory |
Publisher | : |
Total Pages | : 372 |
Release | : 1961 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Handbook of Supersonic Aerodynamics Book in PDF, ePub and Kindle
Author | : George D. Catalano |
Publisher | : |
Total Pages | : 62 |
Release | : 2001-09 |
Genre | : |
ISBN | : 9781423550181 |
Download A Numerical Investigation of Subsonic and Supersonic Flow Around Axisymmetric Bodies Book in PDF, ePub and Kindle
A computational fluid dynamics (CFD) approach to predicting high- speed aerodynamic flow fields of interest to the U.S. Army Research Laboratory (ARL) has been carried out The aerodynamic problems of particular interest are: (1) supersonic flow past the aftbody of projectiles with base mass injection, (2) supersonic flow past the M549 projectile, and (3) subsonic, transonic, and supersonic flow past an M864 projectile with base bleed and wake combustion. The commercially available FLUENT (Fluent, Inc. FLUENT. Version 5.1.1, Lebanon, NH, 1999.) CFD code was utilized. The computational effort supports an ongoing ARL- sponsored experimental investigation. Of particular interest in the present investigation is the careful characterization of the various turbulence models employed in the CFD code. Additionally, the ease of use and set-up as well as the computational time will be described. An experimental effort (Dutton, J. C., and A. L. Addy. 'Fluid Dynamic Mechanisms and Interactions Within Separated Flows'. U.S. Army Research Office Research Grant DAAH04-93-G-0226 and the Department of Mechanical and Industrial Engineering, University of illinois, Urbana-Champagne, Urbana, IL, August 1998.) consisting of detailed laser Doppler velocimeter (LDV), particle image velocimeter (PIV), and high-speed wall pressure measurements has been made in axisymmetric and planar subsonic and supersonic flows with embedded separated regions. The present work seeks to predict similar flow fields computationally and to address areas of agreement and disagreement.
Author | : |
Publisher | : |
Total Pages | : |
Release | : 2014 |
Genre | : |
ISBN | : |
Download Numerical Investigation on Staged Sonic Jet Interaction Mechanism in a Supersonic Cross Flow Book in PDF, ePub and Kindle