Evolution of Large-scale Turbulent Structures in Coannular Supersonic Jets

Evolution of Large-scale Turbulent Structures in Coannular Supersonic Jets
Author :
Publisher :
Total Pages : 144
Release :
ISBN-10 : OCLC:40190421
ISBN-13 :
Rating : 4/5 (21 Downloads)

Book Synopsis Evolution of Large-scale Turbulent Structures in Coannular Supersonic Jets by : Erina Murakami

Download or read book Evolution of Large-scale Turbulent Structures in Coannular Supersonic Jets written by Erina Murakami and published by . This book was released on 1998 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:


Evolution of Large-scale Turbulent Structures in Coannular Supersonic Jets Related Books

Evolution of Large-scale Turbulent Structures in Coannular Supersonic Jets
Language: en
Pages: 144
Authors: Erina Murakami
Categories: Airplanes
Type: BOOK - Published: 1998 - Publisher:

DOWNLOAD EBOOK

Large Scale Turbulent Structures in Supersonic Jets
Language: en
Pages: 34
Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-07-05 - Publisher: Createspace Independent Publishing Platform

DOWNLOAD EBOOK

Jet noise is a major concern in the design of commercial aircraft. Studies by various researchers suggest that aerodynamic noise is a major contributor to jet n
Effect of Swirl on Turbulent Structures in Supersonic Jets
Language: en
Pages: 36
Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-07-02 - Publisher: Createspace Independent Publishing Platform

DOWNLOAD EBOOK

Direct Numerical Simulation (DNS) is used to study the mechanism of generation and evolution of turbulence structures in a temporally evolving supersonic swirli
Coherent Large-scale Structures in High Reynolds Number Supersonic Jets
Language: en
Pages: 112
Authors: J. Lepicovsky
Categories: Aerodynamic noise
Type: BOOK - Published: 1985 - Publisher:

DOWNLOAD EBOOK

The flow structure of a 50.8 mm (2 in) diameter jet operated at a full expanded Mach number of 1.37, with Reynolds numbers in the range 1.7 to 2.35 million, was
Direct Numerical Simulation of Turbulent Supersonic Jets
Language: en
Pages: 264
Authors: Ram Mohan Rao
Categories:
Type: BOOK - Published: 1997 - Publisher:

DOWNLOAD EBOOK